[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
December 10th 2017
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17659 2714 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 582 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
344/22:38:30
000 0
0 0
0 0
0
N/A 0
0 0
0 220
3
000/00:00:00
000 0
0 0
0 215
4
346/16:46:55
000 0
0 0
0 0
0
N/A 0
0 0
0 220
3
000/00:00:00
000 0
0 0
0 215
4
348/01:30:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
2
000/00:00:00
000 0
0 0
0 215
5
348/05:14:30
000 0
0 0
0 0
0
N/A 0
0 0
0 220
1
000/00:00:00
000 0
0 0
0 215
6
349/11:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
1
000/00:00:00
000 0
0 0
0 215
6
351/07:21:00
000 0
0 0
0 0
0
N/A 0
0 0
0 219
9
000/00:00:00
000 0
0 0
0 215
6
353/08:42:47
000 0
0 0
0 0
0
N/A 0
0 0
0 220
0
000/00:00:00
000 0
0 0
0 215
7
Coasting Arc #1 (Orbit 885)
---------------------------------------
Vector Time (GMT): 2017/342/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 919742
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3786448
06 A = 6777339
71 meter
Y = -1934218
67 meter E =
0003237
Z = 5277316
11 I = 51
26823
XDOT = 3084
769984 Wp = 169
11722
YDOT = 7012
683062 meter/sec RA = 248
37871 deg
ZDOT = 353
789888 TA = 277
47422
MA = 277
51099
Ha = 220
433 n
mi
Hp = 215
294
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12422729
86 X = 3782161
03
Y = -6345861
79 feet Y = -1891900
35 meter
Z = 17314029
24 Z = 5295698
93
XDOT = 10120
636429 XDOT = 3004
404480
YDOT = 23007
490362 feet/sec YDOT = 7046
729694 meter/sec
ZDOT = 1160
727980 ZDOT = 368
579995
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3311186
70 X = 1009249
71
Y = 13445770
49 feet Y = 4098270
85 meter
Z = 17395892
80 Z = 5302268
12
XDOT = -23747
037536 XDOT = -7238
097041
YDOT = 4249
387046 feet/sec YDOT = 1295
213172 meter/sec
ZDOT = 1225
292013 ZDOT = 373
469006
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 17342
54887608
00016717 00000-0 10270-3 0 9000
2 25544 51
6404 249
1090 0003068 217
9282 142
1654 15
54147000 8867
Satellite: ISS
Catalog Number: 25544
Epoch time: 17342
54887608 = yrday
fracday
Element set: 900
Inclination: 51
6404 deg
RA of node: 249
1090 deg
Eccentricity:
0003068
Arg of perigee: 217
9282 deg
Mean anomaly: 142
1654 deg
Mean motion: 15
54147000 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 886
Checksum: 301
Coasting Arc #2 (Orbit 900)
---------------------------------------
Vector Time (GMT): 2017/343/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 919742
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4459395
21 A = 6778162
09 meter
Y = 245794
83 meter E =
0012477
Z = -5109826
07 I = 51
28462
XDOT = -2192
451238 Wp = 113
68403
YDOT = -7169
410620 meter/sec RA = 243
35332 deg
ZDOT = 1566
634890 TA = 171
52420
MA = 171
50310
Ha = 220
535 n
mi
Hp = 215
169
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14630561
72 X = -4436991
31
Y = 806413
48 feet Y = 196052
35 meter
Z = -16764521
22 Z = -5131433
99
XDOT = -7193
081488 XDOT = -2119
727956
YDOT = -23521
688387 feet/sec YDOT = -7193
521566 meter/sec
ZDOT = 5139
878249 ZDOT = 1556
160924
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2343877
76 X = 714413
94
Y = -14352156
62 feet Y = -4374537
34 meter
Z = -16860446
26 Z = -5139064
02
XDOT = 23479
500701 XDOT = 7156
551814
YDOT = -2157
512233 feet/sec YDOT = -657
609729 meter/sec
ZDOT = 5094
468648 ZDOT = 1552
794044
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 17343
51341512
00016717 00000-0 10270-3 0 9018
2 25544 51
6412 244
3004 0002894 220
8200 139
2736 15
54126308 9011
Satellite: ISS
Catalog Number: 25544
Epoch time: 17343
51341512 = yrday
fracday
Element set: 901
Inclination: 51
6412 deg
RA of node: 244
3004 deg
Eccentricity:
0002894
Arg of perigee: 220
8200 deg
Mean anomaly: 139
2736 deg
Mean motion: 15
54126308 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 901
Checksum: 263
Coasting Arc #3 (Orbit 916)
---------------------------------------
Vector Time (GMT): 2017/344/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 919742
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4976132
74 A = 6780972
11 meter
Y = 1362512
12 meter E =
0006789
Z = 4395255
01 I = 51
30908
XDOT = 1076
876326 Wp = 79
88950
YDOT = 6825
948148 meter/sec RA = 238
33542 deg
ZDOT = -3329
645585 TA = 43
92578
MA = 43
87183
Ha = 220
291 n
mi
Hp = 215
355
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16325894
83 X = 4939176
90
Y = 4470184
12 feet Y = 1417951
83 meter
Z = 14420127
98 Z = 4419337
86
XDOT = 3533
058813 XDOT = 1016
640519
YDOT = 22394
843004 feet/sec YDOT = 6837
653849 meter/sec
ZDOT = -10924
034072 ZDOT = -3324
560475
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7607780
53 X = -2318851
51
Y = 15018356
78 feet Y = 4577595
15 meter
Z = 14526806
75 Z = 4427770
70
XDOT = -21568
481504 XDOT = -6574
073163
YDOT = -362
672394 feet/sec YDOT = -110
542546 meter/sec
ZDOT = -10902
470457 ZDOT = -3323
072995
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 17344
54225286
00016717 00000-0 10270-3 0 9022
2 25544 51
6405 239
1725 0002836 225
3350 134
7572 15
54140223 9174
Satellite: ISS
Catalog Number: 25544
Epoch time: 17344
54225286 = yrday
fracday
Element set: 902
Inclination: 51
6405 deg
RA of node: 239
1725 deg
Eccentricity:
0002836
Arg of perigee: 225
3350 deg
Mean anomaly: 134
7572 deg
Mean motion: 15
54140223 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 917
Checksum: 290
Coasting Arc #4 (Orbit 923)
---------------------------------------
Vector Time (GMT): 2017/344/22:38:30
000
Vector Time (MET): N/A
Weight (LBS) : 919742
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3259132
77 A = 6777320
95 meter
Y = -2730227
74 meter E =
0003362
Z = 5277857
69 I = 51
30510
XDOT = 4527
429667 Wp = 175
81685
YDOT = 6177
325377 meter/sec RA = 236
13840 deg
ZDOT = 396
474745 TA = 270
36593
MA = 270
40446
Ha = 220
335 n
mi
Hp = 215
422
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10692692
82 X = 3263783
36
Y = -8957440
08 feet Y = -2693756
08 meter
Z = 17315806
06 Z = 5293700
78
XDOT = 14853
771873 XDOT = 4456
090783
YDOT = 20266
815542 feet/sec YDOT = 6227
555296 meter/sec
ZDOT = 1300
770160 ZDOT = 418
294628
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2132647
38 X = -650030
92
Y = -13695522
03 feet Y = -4174395
12 meter
Z = 17386519
01 Z = 5299410
99
XDOT = 24034
525904 XDOT = 7325
723495
YDOT = -1955
765427 feet/sec YDOT = -596
117302 meter/sec
ZDOT = 1396
706154 ZDOT = 425
716036
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 17344
99236677
00016717 00000-0 10270-3 0 9038
2 25544 51
6409 236
9246 0003372 222
3896 137
6996 15
54158287 9248
Satellite: ISS
Catalog Number: 25544
Epoch time: 17344
99236677 = yrday
fracday
Element set: 903
Inclination: 51
6409 deg
RA of node: 236
9246 deg
Eccentricity:
0003372
Arg of perigee: 222
3896 deg
Mean anomaly: 137
6996 deg
Mean motion: 15
54158287 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 924
Checksum: 350
Coasting Arc #5 (Orbit 938)
---------------------------------------
Vector Time (GMT): 2017/345/22:38:30
000
Vector Time (MET): N/A
Weight (LBS) : 919742
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4281867
98 A = 6778057
00 meter
Y = 1220230
64 meter E =
0012114
Z = -5121380
12 I = 51
32658
XDOT = -3694
509600 Wp = 114
37458
YDOT = -6532
667066 meter/sec RA = 231
11668 deg
ZDOT = 1530
368501 TA = 170
46500
MA = 170
44198
Ha = 220
360 n
mi
Hp = 215
323
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14048123
31 X = -4270317
39
Y = 4003381
38 feet Y = 1172412
65 meter
Z = -16802428
23 Z = -5142152
14
XDOT = -12121
094489 XDOT = -3628
618804
YDOT = -21432
634730 feet/sec YDOT = -6573
613240 meter/sec
ZDOT = 5020
894033 ZDOT = 1512
581391
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3604728
45 X = -1098721
23
Y = 14045286
33 feet Y = 4281003
27 meter
Z = -16894800
68 Z = -5149535
25
XDOT = -23611
543096 XDOT = -7196
798336
YDOT = -106
201906 feet/sec YDOT = -32
370341 meter/sec
ZDOT = 4942
890952 ZDOT = 1506
593162
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 17345
95689852
00016717 00000-0 10270-3 0 9043
2 25544 51
6409 232
1171 0003246 226
7446 133
3436 15
54146269 9397
Satellite: ISS
Catalog Number: 25544
Epoch time: 17345
95689852 = yrday
fracday
Element set: 904
Inclination: 51
6409 deg
RA of node: 232
1171 deg
Eccentricity:
0003246
Arg of perigee: 226
7446 deg
Mean anomaly: 133
3436 deg
Mean motion: 15
54146269 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 939
Checksum: 324
Coasting Arc #6 (Orbit 950)
---------------------------------------
Vector Time (GMT): 2017/346/16:46:55
000
Vector Time (MET): N/A
Weight (LBS) : 919742
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3514758
97 A = 6788273
66 meter
Y = 5601089
77 meter E =
0008798
Z = -1512731
36 I = 51
37354
XDOT = -4855
601298 Wp = 161
76967
YDOT = 1500
727162 meter/sec RA = 227
35856 deg
ZDOT = -5742
374819 TA = 34
81632
MA = 34
75879
Ha = 220
278 n
mi
Hp = 215
430
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11531361
44 X = 3459213
02
Y = 18376278
76 feet Y = 5640083
70 meter
Z = -4963029
39 Z = -1495792
27
XDOT = -15930
450454 XDOT = -4844
128090
YDOT = 4923
645545 feet/sec YDOT = 1446
492915 meter/sec
ZDOT = -18839
812397 ZDOT = -5765
934082
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1747222
08 X = 532553
29
Y = 21641163
15 feet Y = 6596226
53 meter
Z = -4888645
09 Z = -1490059
02
XDOT = -14711
518552 XDOT = -4484
070855
YDOT = -3078
767052 feet/sec YDOT = -938
408197 meter/sec
ZDOT = -18944
601650 ZDOT = -5774
314583
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 17346
72852110
00016717 00000-0 10270-3 0 9059
2 25544 51
6377 228
2689 0002873 232
4909 127
5983 15
54167178 9512
Satellite: ISS
Catalog Number: 25544
Epoch time: 17346
72852110 = yrday
fracday
Element set: 905
Inclination: 51
6377 deg
RA of node: 228
2689 deg
Eccentricity:
0002873
Arg of perigee: 232
4909 deg
Mean anomaly: 127
5983 deg
Mean motion: 15
54167178 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 951
Checksum: 335
Coasting Arc #7 (Orbit 966)
---------------------------------------
Vector Time (GMT): 2017/347/16:46:55
000
Vector Time (MET): N/A
Weight (LBS) : 919742
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2462892
18 A = 6785387
21 meter
Y = -5536833
98 meter E =
0010604
Z = 3044156
03 I = 51
38540
XDOT = 5897
416645 Wp = 92
77209
YDOT = 79
980042 meter/sec RA = 222
36473 deg
ZDOT = 4901
504776 TA = 302
29223
MA = 302
39491
Ha = 220
301 n
mi
Hp = 215
525
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8080354
91 X = -2415581
92
Y = -18165465
82 feet Y = -5564111
37 meter
Z = 9987388
56 Z = 3032306
55
XDOT = 19348
479805 XDOT = 5872
274640
YDOT = 262
401714 feet/sec YDOT = 145
788134 meter/sec
ZDOT = 16081
052414 ZDOT = 4930
091817
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 842896
93 X = 256914
99
Y = -19889647
43 feet Y = -6062364
54 meter
Z = 9935575
68 Z = 3028363
47
XDOT = 15640
117353 XDOT = 4767
107769
YDOT = 8784
458191 feet/sec YDOT = 2677
502857 meter/sec
ZDOT = 16207
944101 ZDOT = 4940
181362
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 17347
75734962
00016717 00000-0 10270-3 0 9068
2 25544 51
6365 223
1398 0003095 231
7953 128
2922 15
54147604 9678
Satellite: ISS
Catalog Number: 25544
Epoch time: 17347
75734962 = yrday
fracday
Element set: 906
Inclination: 51
6365 deg
RA of node: 223
1398 deg
Eccentricity:
0003095
Arg of perigee: 231
7953 deg
Mean anomaly: 128
2922 deg
Mean motion: 15
54147604 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 967
Checksum: 330
Coasting Arc #8 (Orbit 971)
---------------------------------------
Vector Time (GMT): 2017/348/01:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 919742
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2652020
88 A = 6777379
43 meter
Y = 3304934
67 meter E =
0012485
Z = -5300076
44 I = 51
37108
XDOT = -5881
656118 Wp = 96
51759
YDOT = -4905
138556 meter/sec RA = 220
52825 deg
ZDOT = -117
265376 TA = 172
36899
MA = 172
34997
Ha = 220
249 n
mi
Hp = 215
451
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8700855
90 X = -2663035
01
Y = 10842961
52 feet Y = 3275216
70 meter
Z = -17388702
22 Z = -5312985
81
XDOT = -19296
772041 XDOT = -5825
798781
YDOT = -16092
974264 feet/sec YDOT = -4970
598931 meter/sec
ZDOT = -384
728923 ZDOT = -145
701559
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12650713
76 X = 3855937
55
Y = 5587610
88 feet Y = 1703103
80 meter
Z = -17446481
56 Z = -5317687
58
XDOT = -10322
956377 XDOT = -3146
437104
YDOT = 21795
222921 feet/sec YDOT = 6643
183946 meter/sec
ZDOT = -510
269667 ZDOT = -155
530194
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 17348
07885818
00016717 00000-0 10270-3 0 9072
2 25544 51
6403 221
5407 0002953 236
0572 124
0300 15
54123068 9729
Satellite: ISS
Catalog Number: 25544
Epoch time: 17348
07885818 = yrday
fracday
Element set: 907
Inclination: 51
6403 deg
RA of node: 221
5407 deg
Eccentricity:
0002953
Arg of perigee: 236
0572 deg
Mean anomaly: 124
0300 deg
Mean motion: 15
54123068 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 972
Checksum: 295
Coasting Arc #9 (Orbit 974)
---------------------------------------
Vector Time (GMT): 2017/348/05:14:30
000
Vector Time (MET): N/A
Weight (LBS) : 904510
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -92262
32 A = 6780023
84 meter
Y = -4921147
60 meter E =
0006907
Z = 4661162
92 I = 51
38098
XDOT = 6641
507924 Wp = 137
02205
YDOT = 2574
120992 meter/sec RA = 219
76953 deg
ZDOT = 2841
705281 TA = 284
62792
MA = 284
70450
Ha = 220
123 n
mi
Hp = 215
568
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -302697
90 X = -59867
74
Y = -16145497
38 feet Y = -4921998
51 meter
Z = 15292529
28 Z = 4660793
11
XDOT = 21789
724160 XDOT = 6598
426051
YDOT = 8445
278845 feet/sec YDOT = 2648
149807 meter/sec
ZDOT = 9323
180055 ZDOT = 2873
863522
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4921154
97 X = -1499968
03
Y = 15381149
87 feet Y = 4688174
48 meter
Z = 15291586
77 Z = 4660875
65
XDOT = -16627
256429 XDOT = -5067
987760
YDOT = -14754
615260 feet/sec YDOT = -4497
206731 meter/sec
ZDOT = 9465
578546 ZDOT = 2885
108341
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 17348
27176228
00016717 00000-0 10270-3 0 9083
2 25544 51
6372 220
5798 0002996 240
4679 119
6175 15
54158890 9754
Satellite: ISS
Catalog Number: 25544
Epoch time: 17348
27176228 = yrday
fracday
Element set: 908
Inclination: 51
6372 deg
RA of node: 220
5798 deg
Eccentricity:
0002996
Arg of perigee: 240
4679 deg
Mean anomaly: 119
6175 deg
Mean motion: 15
54158890 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 975
Checksum: 351
Coasting Arc #10 (Orbit 989)
---------------------------------------
Vector Time (GMT): 2017/349/05:14:30
000
Vector Time (MET): N/A
Weight (LBS) : 904510
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1447879
72 A = 6777695
03 meter
Y = 4075610
00 meter E =
0011638
Z = -5228434
97 I = 51
39934
XDOT = -6660
342377 Wp = 86
70889
YDOT = -3648
638611 meter/sec RA = 214
75482 deg
ZDOT = -1001
012368 TA = 173
67248
MA = 173
65777
Ha = 220
131 n
mi
Hp = 215
517
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4750261
53 X = -1467949
25
Y = 13371423
89 feet Y = 4059307
03 meter
Z = -17153658
04 Z = -5235516
81
XDOT = -21851
516984 XDOT = -6614
184834
YDOT = -11970
599117 feet/sec YDOT = -3722
860949 meter/sec
ZDOT = -3284
161313 ZDOT = -1033
254754
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8578728
64 X = 2614796
49
Y = -11254592
53 feet Y = -3430399
80 meter
Z = -17185677
40 Z = -5238194
47
XDOT = 16181
781852 XDOT = 4932
207108
YDOT = 17560
755903 feet/sec YDOT = 5352
518399 meter/sec
ZDOT = -3426
800180 ZDOT = -1044
488695
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 17349
23628551
00016717 00000-0 10270-3 0 9092
2 25544 51
6377 215
7709 0002844 243
9611 116
1249 15
54135970 9908
Satellite: ISS
Catalog Number: 25544
Epoch time: 17349
23628551 = yrday
fracday
Element set: 909
Inclination: 51
6377 deg
RA of node: 215
7709 deg
Eccentricity:
0002844
Arg of perigee: 243
9611 deg
Mean anomaly: 116
1249 deg
Mean motion: 15
54135970 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 990
Checksum: 324
Coasting Arc #11 (Orbit 993)
---------------------------------------
Vector Time (GMT): 2017/349/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925679
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6080650
34 A = 6788367
52 meter
Y = 2608138
15 meter E =
0012360
Z = 1487106
11 I = 51
44496
XDOT = -737
417787 Wp = 129
10756
YDOT = 5015
516220 meter/sec RA = 213
53508 deg
ZDOT = -5756
617707 TA = 34
60725
MA = 34
52688
Ha = 220
092 n
mi
Hp = 215
606
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19949640
24 X = 6043809
81
Y = 8556883
69 feet Y = 2675930
03 meter
Z = 4878957
04 Z = 1516555
05
XDOT = -2419
349695 XDOT = -765
484734
YDOT = 16455
105709 feet/sec YDOT = 5007
113463 meter/sec
ZDOT = -18886
541033 ZDOT = -5760
267638
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15281866
83 X = -4657913
01
Y = 15374772
78 feet Y = 4686230
74 meter
Z = 5009344
66 Z = 1526848
25
XDOT = -13335
512413 XDOT = -4064
664184
YDOT = -7070
345417 feet/sec YDOT = -2155
041283 meter/sec
ZDOT = -18903
455358 ZDOT = -5761
773193
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 17349
49349168
00016717 00000-0 10270-3 0 9106
2 25544 51
6412 214
4911 0002913 245
0312 115
0538 15
54120181 9948
Satellite: ISS
Catalog Number: 25544
Epoch time: 17349
49349168 = yrday
fracday
Element set: 910
Inclination: 51
6412 deg
RA of node: 214
4911 deg
Eccentricity:
0002913
Arg of perigee: 245
0312 deg
Mean anomaly: 115
0538 deg
Mean motion: 15
54120181 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 994
Checksum: 288
Coasting Arc #12 (Orbit 1009)
---------------------------------------
Vector Time (GMT): 2017/350/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925679
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5874930
66 A = 6789202
98 meter
Y = -3385750
19 meter E =
0009833
Z = 208637
91 I = 51
47538
XDOT = 2549
783311 Wp = 40
04898
YDOT = -4045
724978 meter/sec RA = 208
55136 deg
ZDOT = 5994
416140 TA = 322
20397
MA = 322
27298
Ha = 219
933 n
mi
Hp = 215
658
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19274706
89 X = -5837647
12
Y = -11108104
30 feet Y = -3451239
24 meter
Z = 684507
59 Z = 180189
31
XDOT = 8365
430810 XDOT = 2565
716021
YDOT = -13273
375913 feet/sec YDOT = -4017
123068 meter/sec
ZDOT = 19666
719620 ZDOT = 6006
840596
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17178455
53 X = 5235993
24
Y = -14140771
93 feet Y = -4310107
28 meter
Z = 558652
31 Z = 170277
22
XDOT = 8496
326929 XDOT = 2589
680448
YDOT = 11124
494324 feet/sec YDOT = 3390
745870 meter/sec
ZDOT = 19722
461893 ZDOT = 6011
406385
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 17350
52230896
00016717 00000-0 10270-3 0 9110
2 25544 51
6406 209
3616 0002969 252
9983 107
0844 15
54168061 10108
Satellite: ISS
Catalog Number: 25544
Epoch time: 17350
52230896 = yrday
fracday
Element set: 911
Inclination: 51
6406 deg
RA of node: 209
3616 deg
Eccentricity:
0002969
Arg of perigee: 252
9983 deg
Mean anomaly: 107
0844 deg
Mean motion: 15
54168061 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1010
Checksum: 302
Coasting Arc #13 (Orbit 1022)
---------------------------------------
Vector Time (GMT): 2017/351/07:21:00
000
Vector Time (MET): N/A
Weight (LBS) : 925679
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -534624
44 A = 6778722
57 meter
Y = -4582451
17 meter E =
0004833
Z = 4965834
57 I = 51
46297
XDOT = 7234
748117 Wp = 150
59845
YDOT = 1436
137103 meter/sec RA = 204
32920 deg
ZDOT = 2099
160482 TA = 278
89037
MA = 278
94509
Ha = 219
913 n
mi
Hp = 215
636
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1754017
19 X = -507464
23
Y = -15034288
63 feet Y = -4588278
39 meter
Z = 16292108
17 Z = 4963302
98
XDOT = 23736
050253 XDOT = 7207
954393
YDOT = 4711
735902 feet/sec YDOT = 1516
890959 meter/sec
ZDOT = 6887
009455 ZDOT = 2134
239939
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5809749
33 X = 1770811
60
Y = 13989229
06 feet Y = 4263917
02 meter
Z = 16281507
38 Z = 4962603
45
XDOT = -23067
973363 XDOT = -7031
118281
YDOT = 1364
463160 feet/sec YDOT = 415
888371 meter/sec
ZDOT = 7042
604709 ZDOT = 2146
585915
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 17351
35822377
00016717 00000-0 10270-3 0 9124
2 25544 51
6384 205
1942 0002982 254
5994 105
4829 15
54181910 10231
Satellite: ISS
Catalog Number: 25544
Epoch time: 17351
35822377 = yrday
fracday
Element set: 912
Inclination: 51
6384 deg
RA of node: 205
1942 deg
Eccentricity:
0002982
Arg of perigee: 254
5994 deg
Mean anomaly: 105
4829 deg
Mean motion: 15
54181910 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1023
Checksum: 309
Coasting Arc #14 (Orbit 1037)
---------------------------------------
Vector Time (GMT): 2017/352/07:21:00
000
Vector Time (MET): N/A
Weight (LBS) : 925679
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1198639
27 A = 6777263
19 meter
Y = 4054792
73 meter E =
0012014
Z = -5306934
08 I = 51
48882
XDOT = -7274
053731 Wp = 90
64087
YDOT = -2393
096283 meter/sec RA = 199
31834 deg
ZDOT = -186
016801 TA = 177
58356
MA = 177
57775
Ha = 219
915 n
mi
Hp = 215
582
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3932543
54 X = -1218113
41
Y = 13303125
76 feet Y = 4041280
46 meter
Z = -17411201
05 Z = -5312803
54
XDOT = -23865
005680 XDOT = -7245
849283
YDOT = -7851
365757 feet/sec YDOT = -2474
282001 meter/sec
ZDOT = -610
291343 ZDOT = -221
283776
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -112630
97 X = -34329
92
Y = -13838246
03 feet Y = -4217897
39 meter
Z = -17437839
22 Z = -5315053
39
XDOT = 24098
471415 XDOT = 7345
214087
YDOT = 767
830921 feet/sec YDOT = 234
034865 meter/sec
ZDOT = -766
611057 ZDOT = -233
663050
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 17352
32273907
00016717 00000-0 10270-3 0 9132
2 25544 51
6390 200
3854 0002872 259
8310 100
2519 15
54166528 10388
Satellite: ISS
Catalog Number: 25544
Epoch time: 17352
32273907 = yrday
fracday
Element set: 913
Inclination: 51
6390 deg
RA of node: 200
3854 deg
Eccentricity:
0002872
Arg of perigee: 259
8310 deg
Mean anomaly: 100
2519 deg
Mean motion: 15
54166528 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1038
Checksum: 294
Coasting Arc #15 (Orbit 1053)
---------------------------------------
Vector Time (GMT): 2017/353/07:21:00
000
Vector Time (MET): N/A
Weight (LBS) : 925679
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2911288
90 A = 6778143
24 meter
Y = -3420583
72 meter E =
0003063
Z = 5075687
90 I = 51
52319
XDOT = 6765
592258 Wp = 26
38143
YDOT = 3159
659027 meter/sec RA = 194
31005 deg
ZDOT = -1748
139707 TA = 80
56429
MA = 80
52967
Ha = 219
749 n
mi
Hp = 215
640
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9551472
77 X = 2924667
23
Y = -11222387
54 feet Y = -3387953
49 meter
Z = 16652519
36 Z = 5089862
13
XDOT = 22196
824995 XDOT = 6738
248869
YDOT = 10366
335390 feet/sec YDOT = 3235
163822 meter/sec
ZDOT = -5735
366493 ZDOT = -1715
340618
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5638355
14 X = -1718570
65
Y = 13537519
65 feet Y = 4126235
99 meter
Z = 16715966
27 Z = 5095026
52
XDOT = -23333
060875 XDOT = -7111
916955
YDOT = -2803
119418 feet/sec YDOT = -854
390799 meter/sec
ZDOT = -5590
090522 ZDOT = -1703
859591
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 17353
35154969
00016717 00000-0 10270-3 0 9143
2 25544 51
6388 195
2570 0002921 266
0165 94
0654 15
54186098 10547
Satellite: ISS
Catalog Number: 25544
Epoch time: 17353
35154969 = yrday
fracday
Element set: 914
Inclination: 51
6388 deg
RA of node: 195
2570 deg
Eccentricity:
0002921
Arg of perigee: 266
0165 deg
Mean anomaly: 94
0654 deg
Mean motion: 15
54186098 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1054
Checksum: 324
Coasting Arc #16 (Orbit 1054)
---------------------------------------
Vector Time (GMT): 2017/353/08:42:47
000
Vector Time (MET): N/A
Weight (LBS) : 940911
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1866184
54 A = 6779495
94 meter
Y = -4402599
77 meter E =
0005316
Z = 4804270
34 I = 51
53038
XDOT = 7227
990829 Wp = 136
98207
YDOT = -277
098745 meter/sec RA = 194
06016 deg
ZDOT = 2548
256720 TA = 287
87631
MA = 287
93428
Ha = 219
964 n
mi
Hp = 215
658
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6122652
70 X = -1840151
56
Y = -14444224
98 feet Y = -4423323
73 meter
Z = 15762041
79 Z = 4795267
71
XDOT = 23713
880672 XDOT = 7218
174054
YDOT = -909
116619 feet/sec YDOT = -196
325599 meter/sec
ZDOT = 8360
422310 ZDOT = 2583
344157
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13794114
80 X = 4204446
19
Y = 7555455
07 feet Y = 2302902
71 meter
Z = 15722657
81 Z = 4792266
10
XDOT = -17541
205866 XDOT = -5346
559548
YDOT = 14265
560712 feet/sec YDOT = 4348
142905 meter/sec
ZDOT = 8516
343820 ZDOT = 2595
781596
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 17353
41585080
00016717 00000-0 10270-3 0 9153
2 25544 51
6402 194
9362 0002843 264
5025 95
5803 15
54158556 10551
Satellite: ISS
Catalog Number: 25544
Epoch time: 17353
41585080 = yrday
fracday
Element set: 915
Inclination: 51
6402 deg
RA of node: 194
9362 deg
Eccentricity:
0002843
Arg of perigee: 264
5025 deg
Mean anomaly: 95
5803 deg
Mean motion: 15
54158556 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1055
Checksum: 308
Coasting Arc #17 (Orbit 1069)
---------------------------------------
Vector Time (GMT): 2017/354/08:42:47
000
Vector Time (MET): N/A
Weight (LBS) : 940911
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 84569
88 A = 6777355
39 meter
Y = 4259119
54 meter E =
0011694
Z = -5281362
03 I = 51
55495
XDOT = -7601
014481 Wp = 83
60274
YDOT = -675
627097 meter/sec RA = 189
05581 deg
ZDOT = -666
565575 TA = 180
01818
MA = 180
01822
Ha = 219
831 n
mi
Hp = 215
632
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 277460
23 X = 62591
13
Y = 13973489
31 feet Y = 4259942
96 meter
Z = -17327303
25 Z = -5281004
12
XDOT = -24937
711551 XDOT = -7589
656680
YDOT = -2216
624334 feet/sec YDOT = -760
563256 meter/sec
ZDOT = -2186
894931 ZDOT = -703
461288
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9088607
43 X = -2770207
54
Y = -10619194
78 feet Y = -3236730
57 meter
Z = -17326302
05 Z = -5281056
86
XDOT = 20000
521716 XDOT = 6096
159019
YDOT = -13282
265906 feet/sec YDOT = -4048
434648 meter/sec
ZDOT = -2350
744757 ZDOT = -716
507002
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 17354
38035841
00016717 00000-0 10270-3 0 9166
2 25544 51
6395 190
1282 0002932 269
8200 90
2617 15
54186952 10706
Satellite: ISS
Catalog Number: 25544
Epoch time: 17354
38035841 = yrday
fracday
Element set: 916
Inclination: 51
6395 deg
RA of node: 190
1282 deg
Eccentricity:
0002932
Arg of perigee: 269
8200 deg
Mean anomaly: 90
2617 deg
Mean motion: 15
54186952 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1070
Checksum: 306
Coasting Arc #18 (Orbit 1085)
---------------------------------------
Vector Time (GMT): 2017/355/08:42:47
000
Vector Time (MET): N/A
Weight (LBS) : 940911
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1737640
65 A = 6777622
96 meter
Y = -4000653
97 meter E =
0002480
Z = 5187837
09 I = 51
58923
XDOT = 7400
690531 Wp = 7
03660
YDOT = 1545
307047 meter/sec RA = 184
05113 deg
ZDOT = -1284
671603 TA = 95
32218
MA = 95
29389
Ha = 219
675 n
mi
Hp = 215
678
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5700920
75 X = 1757048
10
Y = -13125505
14 feet Y = -3981114
51 meter
Z = 17020462
89 Z = 5196324
67
XDOT = 24280
480746 XDOT = 7389
100721
YDOT = 5069
905010 feet/sec YDOT = 1628
001959 meter/sec
ZDOT = -4214
801847 ZDOT = -1248
749574
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4140369
19 X = 1261984
53
Y = 13650366
23 feet Y = 4160631
63 meter
Z = 17058733
37 Z = 5199501
93
XDOT = -20896
339323 XDOT = -6369
204226
YDOT = 11416
267213 feet/sec YDOT = 3479
678246 meter/sec
ZDOT = -4055
372308 ZDOT = -1236
077479
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 17355
40916398
00016717 00000-0 10270-3 0 9176
2 25544 51
6401 184
9994 0003114 272
9345 87
1451 15
54208120 10863
Satellite: ISS
Catalog Number: 25544
Epoch time: 17355
40916398 = yrday
fracday
Element set: 917
Inclination: 51
6401 deg
RA of node: 184
9994 deg
Eccentricity:
0003114
Arg of perigee: 272
9345 deg
Mean anomaly: 87
1451 deg
Mean motion: 15
54208120 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1086
Checksum: 313
Coasting Arc #19 (Orbit 1100)
---------------------------------------
Vector Time (GMT): 2017/356/08:42:47
000
Vector Time (MET): N/A
Weight (LBS) : 940911
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3439789
22 A = 6780274
10 meter
Y = 3665448
59 meter E =
0007025
Z = -4557279
19 I = 51
63095
XDOT = -6603
364756 Wp = 115
75932
YDOT = -2344
659282 meter/sec RA = 179
05220 deg
ZDOT = 3099
069942 TA = 185
29397
MA = 185
30140
Ha = 219
779 n
mi
Hp = 215
607
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11285397
70 X = -3458384
77
Y = 12025749
96 feet Y = 3626878
95 meter
Z = -14951703
37 Z = -4574033
31
XDOT = -21664
582533 XDOT = -6591
709002
YDOT = -7692
451712 feet/sec YDOT = -2418
437732 meter/sec
ZDOT = 10167
552303 ZDOT = 3067
021215
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 575359
73 X = 175369
65
Y = -16413419
00 feet Y = -5002810
11 meter
Z = -15026674
11 Z = -4580130
27
XDOT = 20260
847012 XDOT = 6175
506169
YDOT = -8465
950393 feet/sec YDOT = -2580
421680 meter/sec
ZDOT = 10025
422951 ZDOT = 3055
748916
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 17356
37366784
00016717 00000-0 10270-3 0 9182
2 25544 51
6403 180
1904 0003109 278
4730 81
6070 15
54186979 11018
Satellite: ISS
Catalog Number: 25544
Epoch time: 17356
37366784 = yrday
fracday
Element set: 918
Inclination: 51
6403 deg
RA of node: 180
1904 deg
Eccentricity:
0003109
Arg of perigee: 278
4730 deg
Mean anomaly: 81
6070 deg
Mean motion: 15
54186979 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1101
Checksum: 314
Coasting Arc #20 (Orbit 1116)
---------------------------------------
Vector Time (GMT): 2017/357/08:42:47
000
Vector Time (MET): N/A
Weight (LBS) : 940911
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4878373
17 A = 6784014
14 meter
Y = -3230146
78 meter E =
0009403
Z = 3426564
96 I = 51
67622
XDOT = 5294
249496 Wp = 84
44634
YDOT = 3104
497137 meter/sec RA = 174
06544 deg
ZDOT = -4599
093126 TA = 55
45017
MA = 55
36146
Ha = 219
757 n
mi
Hp = 215
593
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16005161
30 X = 4897486
55
Y = -10597594
41 feet Y = -3175486
86 meter
Z = 11242011
03 Z = 3450308
54
XDOT = 17369
584962 XDOT = 5281
480625
YDOT = 10185
358062 feet/sec YDOT = 3163
630010 meter/sec
ZDOT = -15088
888210 ZDOT = -4573
406319
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4777159
44 X = -1456078
20
Y = 18527239
46 feet Y = 5647102
59 meter
Z = 11348002
18 Z = 3458871
06
XDOT = -18451
456711 XDOT = -5624
004005
YDOT = 4438
083628 feet/sec YDOT = 1352
727890 meter/sec
ZDOT = -14975
122351 ZDOT = -4564
417293
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 17357
40246806
00016717 00000-0 10270-3 0 9190
2 25544 51
6400 175
0614 0003071 285
3239 74
7575 15
54211551 11170
Satellite: ISS
Catalog Number: 25544
Epoch time: 17357
40246806 = yrday
fracday
Element set: 919
Inclination: 51
6400 deg
RA of node: 175
0614 deg
Eccentricity:
0003071
Arg of perigee: 285
3239 deg
Mean anomaly: 74
7575 deg
Mean motion: 15
54211551 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1117
Checksum: 294
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