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

 
Date: October 29th 2017

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 19170 5245 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 610 ET - UTC (sec) : 68 18 UT1 - UTC (sec) : 0 00

Maneuvers contained within the current ephemeris are as follows:

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


306/03:16:48 099 0 7 1 4 1 4
N/A 1 3 -0 1 222 6
000/00:03:36 198 -0 0 0 0 213 4

307/05:42:30 000 0 0 0 0 0 0
N/A 0 0 0 0 222 6
000/00:00:00 000 0 0 0 0 213 4

310/13:56:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 5
000/00:00:00 000 0 0 0 0 213 3

Coasting Arc #1 (Orbit 232)
---------------------------------------

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

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2431869
70                 A    =         6787135
28  meter
 Y    =        5988368
84  meter          E    =           
0019089
 Z    =        2041199
08                 I    =           52
02382
 XDOT =      -3919
974084                 Wp   =           67
59043
 YDOT =      -3508
032342  meter/sec      RA   =           97
82983  deg
 ZDOT =       5587
036247                 TA   =          314
86983
                                          MA   =          315
02470
                                          Ha   =            222
588  n
mi
                                          Hp   =            212
691

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7978575
14                 X    =        -2508567
82
 Y    =       19646879
39  feet           Y    =         5960745
22  meter
 Z    =        6696847
36                 Z    =         2029199
16
 XDOT =     -12860
807363                 XDOT =       -3907
594536
 YDOT =     -11509
292462  feet/sec       YDOT =       -3551
798810  meter/sec
 ZDOT =      18330
171413                 ZDOT =        5568
024058

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4759259
28                 X    =        -1450622
23
 Y    =      -20681620
07  feet           Y    =        -6303757
80  meter
 Z    =        6642690
58                 Z    =         2024692
09
 XDOT =      15731
568006                 XDOT =        4794
981928
 YDOT =       2276
919792  feet/sec       YDOT =         694
005153  meter/sec
 ZDOT =      18246
311007                 ZDOT =        5561
475595


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   17300
56030215  
00016717  00000-0  10270-3 0  9000
2 25544  51
6376  98
4241 0005160  64
6969 295
4718 15
54287140  2331


Satellite: ISS
Catalog Number: 25544
Epoch time:      17300
56030215   =   yrday
fracday
Element set:     900
Inclination:       51
6376  deg
RA of node:        98
4241  deg
Eccentricity:     
0005160     
Arg of perigee:    64
6969  deg
Mean anomaly:     295
4718  deg
Mean motion:   15
54287140  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             233
Checksum:              295


Coasting Arc #2 (Orbit 247)
---------------------------------------

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

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3034818
17                 A    =         6783516
66  meter
 Y    =       -4916390
80  meter          E    =           
0010323
 Z    =       -3565616
18                 I    =           52
01526
 XDOT =       3256
260307                 Wp   =           76
02757
 YDOT =       5270
136113  meter/sec      RA   =           92
87694  deg
 ZDOT =      -4503
603846                 TA   =          145
75658
                                          MA   =          145
68997
                                          Ha   =            222
597  n
mi
                                          Hp   =            212
666

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9956752
52                 X    =         3106889
30
 Y    =      -16129891
07  feet           Y    =        -4882050
54  meter
 Z    =      -11698215
81                 Z    =        -3550698
52
 XDOT =      10683
268724                 XDOT =        3218
962867
 YDOT =      17290
472811  feet/sec       YDOT =        5306
341137  meter/sec
 ZDOT =     -14775
603168                 ZDOT =       -4487
876472

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1415897
00                 X    =          431565
40
 Y    =       18943802
55  feet           Y    =         5774071
02  meter
 Z    =      -11631257
05                 Z    =        -3545207
15
 XDOT =     -17522
942977                 XDOT =       -5340
993020
 YDOT =      -7702
785695  feet/sec       YDOT =       -2347
809080  meter/sec
 ZDOT =     -14706
591670                 ZDOT =       -4482
569141


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   17301
52473675  
00016717  00000-0  10270-3 0  9019
2 25544  51
6375  93
6158 0005250  67
6626 292
5083 15
54296697  2483


Satellite: ISS
Catalog Number: 25544
Epoch time:      17301
52473675   =   yrday
fracday
Element set:     901
Inclination:       51
6375  deg
RA of node:        93
6158  deg
Eccentricity:     
0005250     
Arg of perigee:    67
6626  deg
Mean anomaly:     292
5083  deg
Mean motion:   15
54296697  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             248
Checksum:              326


Coasting Arc #3 (Orbit 263)
---------------------------------------

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

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3514939
48                 A    =         6779636
28  meter
 Y    =        3439772
13  meter          E    =           
0012398
 Z    =        4656923
16                 I    =           52
00360
 XDOT =      -2548
086883                 Wp   =           98
84752
 YDOT =      -6611
008793  meter/sec      RA   =           87
91227  deg
 ZDOT =       2951
361697                 TA   =          321
90248
                                          MA   =          321
99008
                                          Ha   =            222
610  n
mi
                                          Hp   =            212
603

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11531953
69                 X    =        -3575764
09
 Y    =       11285341
65  feet           Y    =         3400125
82  meter
 Z    =       15278619
28                 Z    =         4639700
50
 XDOT =      -8359
865101                 XDOT =       -2488
307926
 YDOT =     -21689
661393  feet/sec       YDOT =       -6639
168850  meter/sec
 ZDOT =       9682
945201                 ZDOT =        2939
129214

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2457723
47                 X    =          749114
11
 Y    =      -16020321
44  feet           Y    =        -4882993
98  meter
 Z    =       15201644
50                 Z    =         4633461
24
 XDOT =      18641
773135                 XDOT =        5682
012452
 YDOT =      12024
140834  feet/sec       YDOT =        3664
958126  meter/sec
 ZDOT =       9629
658768                 ZDOT =        2935
119992


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   17302
55346046  
00016717  00000-0  10270-3 0  9025
2 25544  51
6380  88
4857 0005029  71
5302 288
6397 15
54322785  2646


Satellite: ISS
Catalog Number: 25544
Epoch time:      17302
55346046   =   yrday
fracday
Element set:     902
Inclination:       51
6380  deg
RA of node:        88
4857  deg
Eccentricity:     
0005029     
Arg of perigee:    71
5302  deg
Mean anomaly:     288
6397  deg
Mean motion:   15
54322785  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             264
Checksum:              315


Coasting Arc #4 (Orbit 278)
---------------------------------------

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

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3941118
75                 A    =         6777160
59  meter
 Y    =       -1677720
78  meter          E    =           
0019533
 Z    =       -5268998
84                 I    =           51
99412
 XDOT =       1739
698146                 Wp   =           79
89002
 YDOT =       7379
705824  meter/sec      RA   =           82
93905  deg
 ZDOT =      -1048
501803                 TA   =          180
09804
                                          MA   =          180
09842
                                          Ha   =            222
585  n
mi
                                          Hp   =            212
624

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12930179
61                 X    =         3985181
19
 Y    =       -5504333
27  feet           Y    =        -1633402
47  meter
 Z    =      -17286741
61                 Z    =        -5249746
66
 XDOT =       5707
671082                 XDOT =        1662
140197
 YDOT =      24211
633280  feet/sec       YDOT =        7398
726597  meter/sec
 ZDOT =      -3439
966544                 ZDOT =       -1040
239599

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6861183
70                 X    =        -2091288
79
 Y    =       12384167
72  feet           Y    =         3774694
32  meter
 Z    =      -17201023
61                 Z    =        -5242871
99
 XDOT =     -18552
791174                 XDOT =       -5654
890750
 YDOT =     -15007
525899  feet/sec       YDOT =       -4574
293894  meter/sec
 ZDOT =      -3404
433205                 ZDOT =       -1037
671241


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   17303
51788438  
00016717  00000-0  10270-3 0  9038
2 25544  51
6390  83
6773 0005254  74
3738 285
7994 15
54320226  2790


Satellite: ISS
Catalog Number: 25544
Epoch time:      17303
51788438   =   yrday
fracday
Element set:     903
Inclination:       51
6390  deg
RA of node:        83
6773  deg
Eccentricity:     
0005254     
Arg of perigee:    74
3738  deg
Mean anomaly:     285
7994  deg
Mean motion:   15
54320226  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             279
Checksum:              332


Coasting Arc #5 (Orbit 294)
---------------------------------------

Vector Time (GMT): 2017/304/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 920041
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4252177
81                 A    =         6777184
70  meter
 Y    =        -202136
16  meter          E    =           
0008758
 Z    =        5266708
98                 I    =           51
98866
 XDOT =       -841
945632                 Wp   =           69
89067
 YDOT =      -7567
234313  meter/sec      RA   =           77
96045  deg
 ZDOT =       -965
961128                 TA   =           29
32580
                                          MA   =           29
27667
                                          Ha   =            222
835  n
mi
                                          Hp   =            212
495

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13950714
59                 X    =        -4275185
02
 Y    =        -663176
38  feet           Y    =         -249815
17  meter
 Z    =       17279228
95                 Z    =         5245996
96
 XDOT =      -2762
288818                 XDOT =        -752
571963
 YDOT =     -24826
884229  feet/sec       YDOT =       -7576
149876  meter/sec
 ZDOT =      -3169
163806                 ZDOT =        -969
833483

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11329694
61                 X    =         3453290
92
 Y    =       -8358706
01  feet           Y    =        -2547733
59  meter
 Z    =       17187322
29                 Z    =         5238695
83
 XDOT =      17179
727716                 XDOT =        5236
381008
 YDOT =      16707
939751  feet/sec       YDOT =        5092
580036  meter/sec
 ZDOT =      -3185
168226                 ZDOT =        -970
839275


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   17304
54659747  
00016717  00000-0  10270-3 0  9043
2 25544  51
6387  78
5469 0005332  77
9751 282
1999 15
54290193  2955


Satellite: ISS
Catalog Number: 25544
Epoch time:      17304
54659747   =   yrday
fracday
Element set:     904
Inclination:       51
6387  deg
RA of node:        78
5469  deg
Eccentricity:     
0005332     
Arg of perigee:    77
9751  deg
Mean anomaly:     282
1999  deg
Mean motion:   15
54290193  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             295
Checksum:              352


Coasting Arc #6 (Orbit 309)
---------------------------------------

Vector Time (GMT): 2017/305/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 920041
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4461897
21                 A    =         6779498
89  meter
 Y    =        2003468
60  meter          E    =           
0015391
 Z    =       -4708908
61                 I    =           51
98933
 XDOT =       -169
501433                 Wp   =          100
31398
 YDOT =       7098
417387  meter/sec      RA   =           72
98647  deg
 ZDOT =       2864
768495                 TA   =          198
01040
                                          MA   =          198
06499
                                          Ha   =            222
590  n
mi
                                          Hp   =            212
601

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14638770
38                 X    =         4462036
37
 Y    =        6573059
70  feet           Y    =         2053365
01  meter
 Z    =      -15449175
24                 Z    =        -4687233
41
 XDOT =       -556
107063                 XDOT =        -262
781199
 YDOT =      23288
770956  feet/sec       YDOT =        7096
000559  meter/sec
 ZDOT =       9398
846768                 ZDOT =        2863
717998

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15508021
56                 X    =        -4726844
97
 Y    =        4466963
75  feet           Y    =         1361530
55  meter
 Z    =      -15353280
75                 Z    =        -4679679
97
 XDOT =     -14202
522498                 XDOT =       -4328
928857
 YDOT =     -17082
170604  feet/sec       YDOT =       -5206
645600  meter/sec
 ZDOT =       9393
058280                 ZDOT =        2863
004164


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   17305
51100890  
00016717  00000-0  10270-3 0  9052
2 25544  51
6392  73
7387 0005177  81
6200 278
5539 15
54324134  3105


Satellite: ISS
Catalog Number: 25544
Epoch time:      17305
51100890   =   yrday
fracday
Element set:     905
Inclination:       51
6392  deg
RA of node:        73
7387  deg
Eccentricity:     
0005177     
Arg of perigee:    81
6200  deg
Mean anomaly:     278
5539  deg
Mean motion:   15
54324134  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             310
Checksum:              291


Coasting Arc #7 (Orbit 319)
---------------------------------------

Vector Time (GMT): 2017/306/03:18:36
198
Vector Time (MET): N/A
Weight (LBS)     : 919890
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3936889
43                 A    =         6777500
47  meter
 Y    =       -1413035
17  meter          E    =           
0018874
 Z    =       -5349021
62                 I    =           51
97624
 XDOT =       2617
308913                 Wp   =           87
04218
 YDOT =       7193
055599  meter/sec      RA   =           69
84604  deg
 ZDOT =         27
204853                 TA   =          183
21025
                                          MA   =          183
22238
                                          Ha   =            222
550  n
mi
                                          Hp   =            213
404

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12916303
91                 X    =         3978381
37
 Y    =       -4635942
14  feet           Y    =        -1368778
55  meter
 Z    =      -17549283
52                 Z    =        -5329796
06
 XDOT =       8586
971498                 XDOT =        2536
547566
 YDOT =      23599
263775  feet/sec       YDOT =        7221
872573  meter/sec
 ZDOT =         89
254768                 ZDOT =          39
722601

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4723246
42                 X    =        -1439645
51
 Y    =      -13000370
79  feet           Y    =        -3962513
02  meter
 Z    =      -17463720
14                 Z    =        -5322941
90
 XDOT =      22594
126382                 XDOT =        6886
689721
 YDOT =      -8397
248458  feet/sec       YDOT =       -2559
481330  meter/sec
 ZDOT =        143
667114                 ZDOT =          43
789736


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   17306
15394788  
00016717  00000-0  10270-3 0  9065
2 25544  51
6415  70
5367 0004104  75
8331 284
3277 15
54080606  3201


Satellite: ISS
Catalog Number: 25544
Epoch time:      17306
15394788   =   yrday
fracday
Element set:     906
Inclination:       51
6415  deg
RA of node:        70
5367  deg
Eccentricity:     
0004104     
Arg of perigee:    75
8331  deg
Mean anomaly:     284
3277  deg
Mean motion:   15
54080606  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             320
Checksum:              300


Coasting Arc #8 (Orbit 335)
---------------------------------------

Vector Time (GMT): 2017/307/03:18:36
198
Vector Time (MET): N/A
Weight (LBS)     : 919890
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4499869
18                 A    =         6778618
77  meter
 Y    =        -282004
23  meter          E    =           
0009640
 Z    =        5055441
71                 I    =           51
96875
 XDOT =      -1722
256237                 Wp   =           64
73444
 YDOT =      -7224
728374  meter/sec      RA   =           64
87012  deg
 ZDOT =      -1929
129472                 TA   =           43
91623
                                          MA   =           43
83965
                                          Ha   =            222
631  n
mi
                                          Hp   =            213
230

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14763350
32                 X    =        -4520938
88
 Y    =        -925210
71  feet           Y    =         -332442
38  meter
 Z    =       16586094
83                 Z    =         5033530
92
 XDOT =      -5650
446972                 XDOT =       -1631
968345
 YDOT =     -23703
177081  feet/sec       YDOT =       -7243
483091  meter/sec
 ZDOT =      -6329
164936                 ZDOT =       -1937
276228

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -569684
56                 X    =         -173639
85
 Y    =       14889699
13  feet           Y    =         4538380
30  meter
 Z    =       16488886
82                 Z    =         5025812
70
 XDOT =     -22477
755356                 XDOT =       -6851
219833
 YDOT =       6212
776942  feet/sec       YDOT =        1893
654412  meter/sec
 ZDOT =      -6364
151748                 ZDOT =       -1939
793453


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   17307
18281902  
00016717  00000-0  10270-3 0  9073
2 25544  51
6421  65
4081 0004054  77
8390 282
3217 15
54119526  3368


Satellite: ISS
Catalog Number: 25544
Epoch time:      17307
18281902   =   yrday
fracday
Element set:     907
Inclination:       51
6421  deg
RA of node:        65
4081  deg
Eccentricity:     
0004054     
Arg of perigee:    77
8390  deg
Mean anomaly:     282
3217  deg
Mean motion:   15
54119526  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             336
Checksum:              295


Coasting Arc #9 (Orbit 336)
---------------------------------------

Vector Time (GMT): 2017/307/05:42:30
000
Vector Time (MET): N/A
Weight (LBS)     : 919890
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4779268
61                 A    =         6782044
56  meter
 Y    =        2336323
45  meter          E    =           
0011458
 Z    =       -4217642
36                 I    =           51
97662
 XDOT =         -4
841355                 Wp   =           98
92437
 YDOT =       6698
891277  meter/sec      RA   =           64
36359  deg
 ZDOT =       3712
160595                 TA   =          209
01671
                                          MA   =          209
08045
                                          Ha   =            222
551  n
mi
                                          Hp   =            213
402

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15680015
14                 X    =         4773275
87
 Y    =        7665103
18  feet           Y    =         2389734
78  meter
 Z    =      -13837409
31                 Z    =        -4194440
13
 XDOT =        -15
883709                 XDOT =         -97
782189
 YDOT =      21977
989753  feet/sec       YDOT =        6698
317660  meter/sec
 ZDOT =      12179
004577                 ZDOT =        3711
910993

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3501131
06                 X    =        -1067144
75
 Y    =      -17181031
09  feet           Y    =        -5236778
28  meter
 Z    =      -13734803
60                 Z    =        -4186368
14
 XDOT =      16257
405279                 XDOT =        4955
257129
 YDOT =     -13029
135758  feet/sec       YDOT =       -3971
280579  meter/sec
 ZDOT =      12176
806721                 ZDOT =        3711
490689


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   17307
24712344  
00016717  00000-0  10270-3 0  9080
2 25544  51
6403  65
0861 0004027  78
2948 281
8656 15
54082661  3375


Satellite: ISS
Catalog Number: 25544
Epoch time:      17307
24712344   =   yrday
fracday
Element set:     908
Inclination:       51
6403  deg
RA of node:        65
0861  deg
Eccentricity:     
0004027     
Arg of perigee:    78
2948  deg
Mean anomaly:     281
8656  deg
Mean motion:   15
54082661  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             337
Checksum:              309


Coasting Arc #10 (Orbit 352)
---------------------------------------

Vector Time (GMT): 2017/308/05:42:30
000
Vector Time (MET): N/A
Weight (LBS)     : 919890
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4860648
23                 A    =         6785752
61  meter
 Y    =       -3694219
72  meter          E    =           
0017108
 Z    =        2945795
03                 I    =           51
97439
 XDOT =       1231
386079                 Wp   =           93
80614
 YDOT =      -5655
300144  meter/sec      RA   =           59
40381  deg
 ZDOT =      -5036
287381                 TA   =           52
71256
                                          MA   =           52
55670
                                          Ha   =            222
533  n
mi
                                          Hp   =            213
265

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15947008
64                 X    =        -4833286
92
 Y    =      -12120143
45  feet           Y    =        -3748421
75  meter
 Z    =        9664681
87                 Z    =         2922249
30
 XDOT =       4039
980573                 XDOT =        1318
998245
 YDOT =     -18554
134332  feet/sec       YDOT =       -5641
040208  meter/sec
 ZDOT =     -16523
252563                 ZDOT =       -5030
092542

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         454441
30                 X    =          138513
71
 Y    =       20074758
31  feet           Y    =         6118786
33  meter
 Z    =        9560784
47                 Z    =         2914127
10
 XDOT =     -15651
564036                 XDOT =       -4770
596718
 YDOT =       8248
036225  feet/sec       YDOT =        2514
001441  meter/sec
 ZDOT =     -16494
821315                 ZDOT =       -5027
621537


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   17308
27598900  
00016717  00000-0  10270-3 0  9095
2 25544  51
6404  59
9582 0004003  80
0034 280
1570 15
54120699  3538


Satellite: ISS
Catalog Number: 25544
Epoch time:      17308
27598900   =   yrday
fracday
Element set:     909
Inclination:       51
6404  deg
RA of node:        59
9582  deg
Eccentricity:     
0004003     
Arg of perigee:    80
0034  deg
Mean anomaly:     280
1570  deg
Mean motion:   15
54120699  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             353
Checksum:              297


Coasting Arc #11 (Orbit 367)
---------------------------------------

Vector Time (GMT): 2017/309/05:42:30
000
Vector Time (MET): N/A
Weight (LBS)     : 919890
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4705235
97                 A    =         6788621
18  meter
 Y    =        4679785
42  meter          E    =           
0011618
 Z    =       -1415716
59                 I    =           51
96566
 XDOT =      -2530
791515                 Wp   =           51
90108
 YDOT =       4294
557700  meter/sec      RA   =           54
45101  deg
 ZDOT =       5824
152756                 TA   =          292
73865
                                          MA   =          292
86139
                                          Ha   =            222
522  n
mi
                                          Hp   =            213
320

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15437125
89                 X    =         4659432
73
 Y    =       15353626
72  feet           Y    =         4732146
48  meter
 Z    =       -4644739
48                 Z    =        -1392970
54
 XDOT =      -8303
121767                 XDOT =       -2606
918096
 YDOT =      14089
756234  feet/sec       YDOT =        4265
831016  meter/sec
 ZDOT =      19108
112718                 ZDOT =        5811
673652

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2043596
15                 X    =          622888
11
 Y    =      -21697532
81  feet           Y    =        -6613408
00  meter
 Z    =       -4544568
07                 Z    =        -1385184
35
 XDOT =      14656
102652                 XDOT =        4467
180088
 YDOT =      -2582
426526  feet/sec       YDOT =        -787
123605  meter/sec
 ZDOT =      19052
002653                 ZDOT =        5807
050409


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   17309
24054663  
00016717  00000-0  10270-3 0  9108
2 25544  51
6398  55
1500 0003914  85
7900 274
3699 15
54090385  3683


Satellite: ISS
Catalog Number: 25544
Epoch time:      17309
24054663   =   yrday
fracday
Element set:     910
Inclination:       51
6398  deg
RA of node:        55
1500  deg
Eccentricity:     
0003914     
Arg of perigee:    85
7900  deg
Mean anomaly:     274
3699  deg
Mean motion:   15
54090385  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             368
Checksum:              315


Coasting Arc #12 (Orbit 383)
---------------------------------------

Vector Time (GMT): 2017/310/05:42:30
000
Vector Time (MET): N/A
Weight (LBS)     : 919890
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4212418
21                 A    =         6789339
31  meter
 Y    =       -5308885
23  meter          E    =           
0014361
 Z    =        -312249
85                 I    =           51
94859
 XDOT =       3873
098452                 Wp   =          124
65186
 YDOT =      -2730
622614  meter/sec      RA   =           49
50245  deg
 ZDOT =      -6028
303598                 TA   =           58
69889
                                          MA   =           58
55835
                                          Ha   =            222
499  n
mi
                                          Hp   =            213
238

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13820269
72                 X    =        -4151222
96
 Y    =      -17417602
47  feet           Y    =        -5355649
20  meter
 Z    =       -1024441
77                 Z    =         -332564
54
 XDOT =      12707
015920                 XDOT =        3932
628538
 YDOT =      -8958
735610  feet/sec       YDOT =       -2686
978002  meter/sec
 ZDOT =     -19777
898944                 ZDOT =       -6009
344203

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4314254
17                 X    =        -1314984
67
 Y    =       21807546
61  feet           Y    =         6646940
21  meter
 Z    =       -1113702
73                 Z    =         -339456
59
 XDOT =     -13552
628512                 XDOT =       -4130
841171
 YDOT =      -3655
401222  feet/sec       YDOT =       -1114
166293  meter/sec
 ZDOT =     -19693
282221                 ZDOT =       -6002
512421


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   17310
26939984  
00016717  00000-0  10270-3 0  9111
2 25544  51
6400  50
0210 0004035  88
0165 272
1449 15
54107772  3849


Satellite: ISS
Catalog Number: 25544
Epoch time:      17310
26939984   =   yrday
fracday
Element set:     911
Inclination:       51
6400  deg
RA of node:        50
0210  deg
Eccentricity:     
0004035     
Arg of perigee:    88
0165  deg
Mean anomaly:     272
1449  deg
Mean motion:   15
54107772  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             384
Checksum:              284


Coasting Arc #13 (Orbit 388)
---------------------------------------

Vector Time (GMT): 2017/310/13:56:00
000
Vector Time (MET): N/A
Weight (LBS)     : 919890
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5039447
74                 A    =         6780724
25  meter
 Y    =         255278
82  meter          E    =           
0013644
 Z    =       -4542823
09                 I    =           51
91417
 XDOT =       2530
160077                 Wp   =          105
05166
 YDOT =       6491
683470  meter/sec      RA   =           47
77507  deg
 ZDOT =       3176
051960                 TA   =          196
72800
                                          MA   =          196
77305
                                          Ha   =            222
531  n
mi
                                          Hp   =            213
271

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16533621
18                 X    =         5058286
01
 Y    =         837528
94  feet           Y    =          311738
82  meter
 Z    =      -14904275
24                 Z    =        -4518296
58
 XDOT =       8301
050121                 XDOT =        2441
952162
 YDOT =      21298
174114  feet/sec       YDOT =        6519
484161  meter/sec
 ZDOT =      10420
117979                 ZDOT =        3188
128958

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5358941
10                 X    =        -1633405
25
 Y    =       15766282
63  feet           Y    =         4805562
95  meter
 Z    =      -14795458
32                 Z    =        -4509655
70
 XDOT =     -21589
629546                 XDOT =       -6580
519086
 YDOT =       2475
501207  feet/sec       YDOT =         754
532768  meter/sec
 ZDOT =      10472
609404                 ZDOT =        3192
051346


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   17310
59091538  
00016717  00000-0  10270-3 0  9122
2 25544  51
6415  48
4186 0004163  93
6631 266
4998 15
54129652  3891


Satellite: ISS
Catalog Number: 25544
Epoch time:      17310
59091538   =   yrday
fracday
Element set:     912
Inclination:       51
6415  deg
RA of node:        48
4186  deg
Eccentricity:     
0004163     
Arg of perigee:    93
6631  deg
Mean anomaly:     266
4998  deg
Mean motion:   15
54129652  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             389
Checksum:              327


Coasting Arc #14 (Orbit 404)
---------------------------------------

Vector Time (GMT): 2017/311/13:56:00
000
Vector Time (MET): N/A
Weight (LBS)     : 919890
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5642936
64                 A    =         6784479
90  meter
 Y    =       -1597515
96  meter          E    =           
0016550
 Z    =        3396156
98                 I    =           51
90404
 XDOT =      -1112
096715                 Wp   =           91
67345
 YDOT =      -6000
651110  meter/sec      RA   =           42
80703  deg
 ZDOT =      -4651
423780                 TA   =           48
77513
                                          MA   =           48
63260
                                          Ha   =            222
541  n
mi
                                          Hp   =            213
189

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18513571
64                 X    =        -5641150
62
 Y    =       -5241194
10  feet           Y    =        -1660609
27  meter
 Z    =       11142247
31                 Z    =         3368749
01
 XDOT =      -3648
611269                 XDOT =       -1022
318334
 YDOT =     -19687
175557  feet/sec       YDOT =       -6012
585184  meter/sec
 ZDOT =     -15260
576705                 ZDOT =       -4656
608278

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9845711
04                 X    =         3000972
73
 Y    =      -16612478
85  feet           Y    =        -5063483
55  meter
 Z    =       11020873
20                 Z    =         3359162
15
 XDOT =      18727
203513                 XDOT =        5708
051631
 YDOT =        918
561938  feet/sec       YDOT =         279
977679  meter/sec
 ZDOT =     -15282
548466                 ZDOT =       -4658
120772


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   17311
61975898  
00016717  00000-0  10270-3 0  9137
2 25544  51
6414  43
2903 0004040  95
7319 264
4298 15
54149837  4057


Satellite: ISS
Catalog Number: 25544
Epoch time:      17311
61975898   =   yrday
fracday
Element set:     913
Inclination:       51
6414  deg
RA of node:        43
2903  deg
Eccentricity:     
0004040     
Arg of perigee:    95
7319  deg
Mean anomaly:     264
4298  deg
Mean motion:   15
54149837  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             405
Checksum:              318


Coasting Arc #15 (Orbit 419)
---------------------------------------

Vector Time (GMT): 2017/312/13:56:00
000
Vector Time (MET): N/A
Weight (LBS)     : 919890
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5926441
01                 A    =         6787843
60  meter
 Y    =        2680730
31  meter          E    =           
0009733
 Z    =       -1937011
60                 I    =           51
88960
 XDOT =       -515
736972                 Wp   =           59
94252
 YDOT =       5183
625266  meter/sec      RA   =           37
84723  deg
 ZDOT =       5621
773954                 TA   =          278
78929
                                          MA   =          278
89949
                                          Ha   =            222
531  n
mi
                                          Hp   =            213
268

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19443704
12                 X    =         5905433
12
 Y    =        8795046
96  feet           Y    =         2746886
43  meter
 Z    =       -6355024
93                 Z    =        -1908273
21
 XDOT =      -1692
050432                 XDOT =        -600
971622
 YDOT =      17006
644575  feet/sec       YDOT =        5177
381175  meter/sec
 ZDOT =      18444
140268                 ZDOT =        5619
061772

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13224567
83                 X    =        -4030848
27
 Y    =       16796440
98  feet           Y    =         5119555
21  meter
 Z    =       -6227936
95                 Z    =        -1898275
18
 XDOT =     -14847
411215                 XDOT =       -4525
490938
 YDOT =      -4887
983614  feet/sec       YDOT =       -1489
857405  meter/sec
 ZDOT =      18431
196536                 ZDOT =        5617
828704


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   17312
58429391  
00016717  00000-0  10270-3 0  9147
2 25544  51
6407  38
4825 0004048  99
2566 260
9045 15
54111912  4200


Satellite: ISS
Catalog Number: 25544
Epoch time:      17312
58429391   =   yrday
fracday
Element set:     914
Inclination:       51
6407  deg
RA of node:        38
4825  deg
Eccentricity:     
0004048     
Arg of perigee:    99
2566  deg
Mean anomaly:     260
9045  deg
Mean motion:   15
54111912  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             420
Checksum:              301


Coasting Arc #16 (Orbit 435)
---------------------------------------

Vector Time (GMT): 2017/313/13:56:00
000
Vector Time (MET): N/A
Weight (LBS)     : 919890
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5786206
49                 A    =         6789223
02  meter
 Y    =       -3531777
71  meter          E    =           
0016186
 Z    =         225015
21                 I    =           51
86898
 XDOT =       2289
402312                 Wp   =          124
27803
 YDOT =      -4153
897202  meter/sec      RA   =           32
89207  deg
 ZDOT =      -6027
308326                 TA   =           53
30479
                                          MA   =           53
15617
                                          Ha   =            222
475  n
mi
                                          Hp   =            213
111

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18983617
11                 X    =        -5747376
20
 Y    =      -11587197
20  feet           Y    =        -3596265
91  meter
 Z    =         738238
89                 Z    =          197001
46
 XDOT =       7511
162441                 XDOT =        2364
960257
 YDOT =     -13628
271661  feet/sec       YDOT =       -4127
872937  meter/sec
 ZDOT =     -19774
633614                 ZDOT =       -6016
003538

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15544161
12                 X    =         4737860
31
 Y    =      -15911859
53  feet           Y    =        -4849934
79  meter
 Z    =         614520
57                 Z    =          187305
87
 XDOT =      10412
952050                 XDOT =        3173
867785
 YDOT =       9364
960268  feet/sec       YDOT =        2854
439890  meter/sec
 ZDOT =     -19723
727720                 ZDOT =       -6011
792209


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   17313
61312171  
00016717  00000-0  10270-3 0  9150
2 25544  51
6414  33
3532 0004226 100
5067 259
6562 15
54160421  4362


Satellite: ISS
Catalog Number: 25544
Epoch time:      17313
61312171   =   yrday
fracday
Element set:     915
Inclination:       51
6414  deg
RA of node:        33
3532  deg
Eccentricity:     
0004226     
Arg of perigee:   100
5067  deg
Mean anomaly:     259
6562  deg
Mean motion:   15
54160421  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             436
Checksum:              266


Coasting Arc #17 (Orbit 451)
---------------------------------------

Vector Time (GMT): 2017/314/13:56:00
000
Vector Time (MET): N/A
Weight (LBS)     : 919890
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5223693
60                 A    =         6788413
42  meter
 Y    =        4070207
14  meter          E    =           
0017378
 Z    =        1461596
01                 I    =           51
83704
 XDOT =      -4001
344487                 Wp   =           70
59118
 YDOT =       3035
312865  meter/sec      RA   =           27
93650  deg
 ZDOT =       5797
606976                 TA   =          305
31808
                                          MA   =          305
48044
                                          Ha   =            222
559  n
mi
                                          Hp   =            213
108

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17138102
37                 X    =         5170691
42
 Y    =       13353697
97  feet           Y    =         4128325
69  meter
 Z    =        4795262
50                 Z    =         1486842
68
 XDOT =     -13127
770627                 XDOT =       -4063
151044
 YDOT =       9958
375541  feet/sec       YDOT =        2990
221484  meter/sec
 ZDOT =      19021
020261                 ZDOT =        5778
019350

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16607116
51                 X    =        -5061849
11
 Y    =       13969943
18  feet           Y    =         4258038
68  meter
 Z    =        4906598
97                 Z    =         1495531
37
 XDOT =      -5980
943859                 XDOT =       -1822
991688
 YDOT =     -13816
714169  feet/sec       YDOT =       -4211
334479  meter/sec
 ZDOT =      18933
548173                 ZDOT =        5770
945483


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   17314
64194350  
00016717  00000-0  10270-3 0  9162
2 25544  51
6405  28
2249 0004300 102
5468 257
6166 15
54119048  4525


Satellite: ISS
Catalog Number: 25544
Epoch time:      17314
64194350   =   yrday
fracday
Element set:     916
Inclination:       51
6405  deg
RA of node:        28
2249  deg
Eccentricity:     
0004300     
Arg of perigee:   102
5468  deg
Mean anomaly:     257
6166  deg
Mean motion:   15
54119048  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             452
Checksum:              291
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