[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
June 28th 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) : 77 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 664 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
182/20:55:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
5
000/00:00:00
000 0
0 0
0 214
8
183/15:38:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
4
000/00:00:00
000 0
0 0
0 214
9
190/12:20:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
1
000/00:00:00
000 0
0 0
0 214
0
Coasting Arc #1 (Orbit 2350)
---------------------------------------
Vector Time (GMT): 2017/179/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922738
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 177663
60 A = 6777990
97 meter
Y = 4321053
60 meter E =
0006457
Z = 5219152
79 I = 51
50351
XDOT = -7421
619736 Wp = 8
86318
YDOT = 1606
079576 meter/sec RA = 341
35051 deg
ZDOT = -1070
643335 TA = 91
44973
MA = 91
37576
Ha = 221
123 n
mi
Hp = 215
446
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 582885
84 X = 103979
46
Y = 14176685
04 feet Y = 4322627
86 meter
Z = 17123204
68 Z = 5219837
26
XDOT = -24349
146117 XDOT = -7433
827156
YDOT = 5269
289949 feet/sec YDOT = 1523
017838 meter/sec
ZDOT = -3512
609366 ZDOT = -1106
724332
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14054322
88 X = 4283757
61
Y = -1928579
41 feet Y = -587831
00 meter
Z = 17125387
10 Z = 5219817
99
XDOT = 7605
541340 XDOT = 2318
169000
YDOT = 22628
818010 feet/sec YDOT = 6897
263729 meter/sec
ZDOT = -3672
214731 ZDOT = -1119
291050
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 17179
54633345
00016717 00000-0 10270-3 0 9005
2 25544 51
6380 341
7106 0004772 333
0174 27
0730 15
54051394 23515
Satellite: ISS
Catalog Number: 25544
Epoch time: 17179
54633345 = yrday
fracday
Element set: 900
Inclination: 51
6380 deg
RA of node: 341
7106 deg
Eccentricity:
0004772
Arg of perigee: 333
0174 deg
Mean anomaly: 27
0730 deg
Mean motion: 15
54051394 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2351
Checksum: 284
Coasting Arc #2 (Orbit 2365)
---------------------------------------
Vector Time (GMT): 2017/180/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922738
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1491018
59 A = 6780266
10 meter
Y = -4701396
62 meter E =
0007900
Z = -4658870
58 I = 51
48265
XDOT = 7076
713772 Wp = 83
41776
YDOT = -600
688629 meter/sec RA = 336
34501 deg
ZDOT = 2876
080966 TA = 215
22382
MA = 215
27606
Ha = 221
128 n
mi
Hp = 215
322
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4891793
28 X = 1566110
32
Y = -15424529
59 feet Y = -4684302
79 meter
Z = -15285008
47 Z = -4651445
74
XDOT = 23217
564870 XDOT = 7068
934421
YDOT = -1970
763219 feet/sec YDOT = -521
595750 meter/sec
ZDOT = 9435
961173 ZDOT = 2910
438179
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15913668
44 X = -4850486
14
Y = -3103148
66 feet Y = -945839
71 meter
Z = -15251323
33 Z = -4648603
35
XDOT = -4962
478694 XDOT = -1512
563506
YDOT = -21590
822534 feet/sec YDOT = -6580
882708 meter/sec
ZDOT = 9587
751340 ZDOT = 2922
346608
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 17180
51088504
00016717 00000-0 10270-3 0 9016
2 25544 51
6397 336
9033 0004804 335
5840 24
5085 15
54096980 23662
Satellite: ISS
Catalog Number: 25544
Epoch time: 17180
51088504 = yrday
fracday
Element set: 901
Inclination: 51
6397 deg
RA of node: 336
9033 deg
Eccentricity:
0004804
Arg of perigee: 335
5840 deg
Mean anomaly: 24
5085 deg
Mean motion: 15
54096980 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2366
Checksum: 312
Coasting Arc #3 (Orbit 2381)
---------------------------------------
Vector Time (GMT): 2017/181/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922738
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3000406
72 A = 6784028
27 meter
Y = 4904321
29 meter E =
0011546
Z = 3597097
45 I = 51
46525
XDOT = -6249
776580 Wp = 63
15002
YDOT = -581
657898 meter/sec RA = 331
34463 deg
ZDOT = -4403
965101 TA = 74
15786
MA = 74
03060
Ha = 221
287 n
mi
Hp = 215
204
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9843854
08 X = -3072497
96
Y = 16090292
96 feet Y = 4870365
35 meter
Z = 11801500
80 Z = 3582347
77
XDOT = -20504
516337 XDOT = -6221
415672
YDOT = -1908
326438 feet/sec YDOT = -651
388223 meter/sec
ZDOT = -14448
704398 ZDOT = -4434
255544
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17299846
19 X = 5272993
12
Y = 7620298
50 feet Y = 2322666
98 meter
Z = 11735449
91 Z = 3576965
13
XDOT = 1463
091569 XDOT = 445
950310
YDOT = 19217
120896 feet/sec YDOT = 5857
378449 meter/sec
ZDOT = -14582
305686 ZDOT = -4444
686773
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 17181
53973813
00016717 00000-0 10270-3 0 9026
2 25544 51
6393 331
7739 0004822 339
5674 20
5285 15
54086724 23824
Satellite: ISS
Catalog Number: 25544
Epoch time: 17181
53973813 = yrday
fracday
Element set: 902
Inclination: 51
6393 deg
RA of node: 331
7739 deg
Eccentricity:
0004822
Arg of perigee: 339
5674 deg
Mean anomaly: 20
5285 deg
Mean motion: 15
54086724 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2382
Checksum: 324
Coasting Arc #4 (Orbit 2396)
---------------------------------------
Vector Time (GMT): 2017/182/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922738
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4175979
84 A = 6787415
35 meter
Y = -4875291
66 meter E =
0009721
Z = -2189543
14 I = 51
44931
XDOT = 5044
245395 Wp = 16
59802
YDOT = 1873
420423 meter/sec RA = 326
35385 deg
ZDOT = 5464
303970 TA = 319
02173
MA = 319
09474
Ha = 221
386 n
mi
Hp = 215
033
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13700721
27 X = 4240821
96
Y = -15995051
36 feet Y = -4828230
29 meter
Z = -7183540
49 Z = -2169100
50
XDOT = 16549
361532 XDOT = 4996
378606
YDOT = 6146
392465 feet/sec YDOT = 1929
560520 meter/sec
ZDOT = 17927
506463 ZDOT = 5488
691154
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17923759
64 X = -5463161
94
Y = -11117182
44 feet Y = -3388517
21 meter
Z = -7092374
80 Z = -2161755
84
XDOT = 2730
711057 XDOT = 832
320730
YDOT = -15876
100377 feet/sec YDOT = -4839
035395 meter/sec
ZDOT = 18034
796754 ZDOT = 5497
006051
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 17182
50428495
00016717 00000-0 10270-3 0 9036
2 25544 51
6400 326
9665 0004853 343
8495 16
2502 15
54103968 23970
Satellite: ISS
Catalog Number: 25544
Epoch time: 17182
50428495 = yrday
fracday
Element set: 903
Inclination: 51
6400 deg
RA of node: 326
9665 deg
Eccentricity:
0004853
Arg of perigee: 343
8495 deg
Mean anomaly: 16
2502 deg
Mean motion: 15
54103968 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2397
Checksum: 320
Coasting Arc #5 (Orbit 2402)
---------------------------------------
Vector Time (GMT): 2017/182/20:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 922738
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3747593
32 A = 6778151
85 meter
Y = -2366963
92 meter E =
0014490
Z = -5140344
56 I = 51
40820
XDOT = 5359
546034 Wp = 57
78852
YDOT = -5266
497983 meter/sec RA = 324
53216 deg
ZDOT = -1477
842081 TA = 197
89171
MA = 197
94278
Ha = 221
487 n
mi
Hp = 214
811
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12295253
66 X = -3695877
57
Y = -7765629
66 feet Y = -2408582
46 meter
Z = -16864647
52 Z = -5158423
75
XDOT = 17583
812448 XDOT = 5425
217681
YDOT = -17278
536688 feet/sec YDOT = -5206
196589 meter/sec
ZDOT = -4848
563257 ZDOT = -1451
648063
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13537441
57 X = 4126212
19
Y = -5053036
26 feet Y = -1540165
45 meter
Z = -16943999
02 Z = -5164530
90
XDOT = 2823
322630 XDOT = 860
548738
YDOT = 23480
527955 feet/sec YDOT = 7156
864921 meter/sec
ZDOT = -4731
940002 ZDOT = -1442
295312
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 17182
89010207
00016717 00000-0 10270-3 0 9047
2 25544 51
6398 325
0477 0005158 346
3516 13
7496 15
54093424 24035
Satellite: ISS
Catalog Number: 25544
Epoch time: 17182
89010207 = yrday
fracday
Element set: 904
Inclination: 51
6398 deg
RA of node: 325
0477 deg
Eccentricity:
0005158
Arg of perigee: 346
3516 deg
Mean anomaly: 13
7496 deg
Mean motion: 15
54093424 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2403
Checksum: 306
Coasting Arc #6 (Orbit 2414)
---------------------------------------
Vector Time (GMT): 2017/183/15:38:00
000
Vector Time (MET): N/A
Weight (LBS) : 901313
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 469470
00 A = 6780698
85 meter
Y = -5046220
46 meter E =
0008005
Z = -4510777
82 I = 51
39813
XDOT = 6631
800560 Wp = 78
89076
YDOT = -2193
376459 meter/sec RA = 320
59600 deg
ZDOT = 3150
231492 TA = 222
81779
MA = 222
88016
Ha = 221
397 n
mi
Hp = 214
868
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1540255
90 X = 547774
39
Y = -16555841
40 feet Y = -5040532
29 meter
Z = -14799139
81 Z = -4508307
54
XDOT = 21757
875853 XDOT = 6640
532323
YDOT = -7196
116993 feet/sec YDOT = -2119
166629 meter/sec
ZDOT = 10335
405157 ZDOT = 3182
467703
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8604858
85 X = -2622760
98
Y = 14239928
54 feet Y = 4340330
22 meter
Z = -14787280
04 Z = -4507162
96
XDOT = -21636
273040 XDOT = -6594
736023
YDOT = -2214
829279 feet/sec YDOT = -675
079964 meter/sec
ZDOT = 10478
107014 ZDOT = 3193
727018
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 17183
66173752
00016717 00000-0 10270-3 0 9059
2 25544 51
6414 321
1997 0004979 346
7640 13
3381 15
54136339 24155
Satellite: ISS
Catalog Number: 25544
Epoch time: 17183
66173752 = yrday
fracday
Element set: 905
Inclination: 51
6414 deg
RA of node: 321
1997 deg
Eccentricity:
0004979
Arg of perigee: 346
7640 deg
Mean anomaly: 13
3381 deg
Mean motion: 15
54136339 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2415
Checksum: 318
Coasting Arc #7 (Orbit 2430)
---------------------------------------
Vector Time (GMT): 2017/184/15:38:00
000
Vector Time (MET): N/A
Weight (LBS) : 901313
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1850587
76 A = 6784530
17 meter
Y = 5584733
14 meter E =
0012656
Z = 3373878
44 I = 51
38690
XDOT = -6072
005751 Wp = 66
77996
YDOT = 787
651278 meter/sec RA = 315
59172 deg
ZDOT = -4615
596784 TA = 73
67725
MA = 73
53810
Ha = 221
581 n
mi
Hp = 214
751
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6071482
15 X = -1929288
82
Y = 18322615
29 feet Y = 5563598
22 meter
Z = 11069154
98 Z = 3364698
27
XDOT = -19921
278712 XDOT = -6057
941890
YDOT = 2584
157735 feet/sec YDOT = 719
829099 meter/sec
ZDOT = -15143
034069 ZDOT = -4645
058469
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13192077
21 X = 4020945
13
Y = -14123342
93 feet Y = -4304794
93 meter
Z = 11027583
67 Z = 3361207
50
XDOT = 18077
089694 XDOT = 5509
896939
YDOT = 4911
588615 feet/sec YDOT = 1497
052210 meter/sec
ZDOT = -15273
217823 ZDOT = -4655
276792
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 17184
69058090
00016717 00000-0 10270-3 0 9061
2 25544 51
6420 316
0707 0005183 350
5888 9
5166 15
54132556 24312
Satellite: ISS
Catalog Number: 25544
Epoch time: 17184
69058090 = yrday
fracday
Element set: 906
Inclination: 51
6420 deg
RA of node: 316
0707 deg
Eccentricity:
0005183
Arg of perigee: 350
5888 deg
Mean anomaly: 9
5166 deg
Mean motion: 15
54132556 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2431
Checksum: 307
Coasting Arc #8 (Orbit 2445)
---------------------------------------
Vector Time (GMT): 2017/185/15:38:00
000
Vector Time (MET): N/A
Weight (LBS) : 901313
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2953086
52 A = 6787915
64 meter
Y = -5797224
29 meter E =
0011453
Z = -1914974
53 I = 51
37457
XDOT = 5190
904488 Wp = 19
42045
YDOT = 804
893810 meter/sec RA = 310
59643 deg
ZDOT = 5588
472507 TA = 319
39181
MA = 319
47718
Ha = 221
758 n
mi
Hp = 214
693
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9688604
08 X = 3026995
14
Y = -19019764
73 feet Y = -5763787
41 meter
Z = -6282724
84 Z = -1900450
51
XDOT = 17030
526535 XDOT = 5154
372106
YDOT = 2640
727723 feet/sec YDOT = 862
737115 meter/sec
ZDOT = 18334
883552 ZDOT = 5613
599672
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16512987
91 X = -5033158
71
Y = 13555685
96 feet Y = 4131773
08 meter
Z = -6217534
85 Z = -1895104
62
XDOT = -13461
433821 XDOT = -4103
045029
YDOT = -7968
548294 feet/sec YDOT = -2428
813520 meter/sec
ZDOT = 18445
634472 ZDOT = 5622
229387
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 17185
65511853
00016717 00000-0 10270-3 0 9070
2 25544 51
6413 311
2630 0005337 353
6153 6
4931 15
54089828 24461
Satellite: ISS
Catalog Number: 25544
Epoch time: 17185
65511853 = yrday
fracday
Element set: 907
Inclination: 51
6413 deg
RA of node: 311
2630 deg
Eccentricity:
0005337
Arg of perigee: 353
6153 deg
Mean anomaly: 6
4931 deg
Mean motion: 15
54089828 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2446
Checksum: 305
Coasting Arc #9 (Orbit 2461)
---------------------------------------
Vector Time (GMT): 2017/186/15:38:00
000
Vector Time (MET): N/A
Weight (LBS) : 901313
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3803633
79 A = 6789302
26 meter
Y = 5616490
78 meter E =
0009640
Z = 222117
21 I = 51
35867
XDOT = -4078
857841 Wp = 109
13469
YDOT = -2517
458299 meter/sec RA = 305
60698 deg
ZDOT = -5981
394960 TA = 68
46387
MA = 68
36115
Ha = 221
796 n
mi
Hp = 214
452
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12479113
48 X = -3867235
11
Y = 18426807
03 feet Y = 5573600
33 meter
Z = 728731
01 Z = 203486
60
XDOT = -13382
079532 XDOT = -4021
349174
YDOT = -8259
377623 feet/sec YDOT = -2562
748542 meter/sec
ZDOT = -19623
999213 ZDOT = -6001
069403
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18593618
47 X = 5667334
91
Y = -12233857
79 feet Y = -3728879
85 meter
Z = 645457
33 Z = 196735
39
XDOT = 8182
146111 XDOT = 2493
918135
YDOT = 11354
683934 feet/sec YDOT = 3460
907663 meter/sec
ZDOT = -19710
365668 ZDOT = -6007
719456
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 17186
68395667
00016717 00000-0 10270-3 0 9088
2 25544 51
6407 306
1347 0005239 359
1739
9404 15
54130920 24626
Satellite: ISS
Catalog Number: 25544
Epoch time: 17186
68395667 = yrday
fracday
Element set: 908
Inclination: 51
6407 deg
RA of node: 306
1347 deg
Eccentricity:
0005239
Arg of perigee: 359
1739 deg
Mean anomaly:
9404 deg
Mean motion: 15
54130920 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2462
Checksum: 318
Coasting Arc #10 (Orbit 2477)
---------------------------------------
Vector Time (GMT): 2017/187/15:38:00
000
Vector Time (MET): N/A
Weight (LBS) : 901313
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4323816
10 A = 6788467
53 meter
Y = -5011535
07 meter E =
0017321
Z = 1460866
43 I = 51
33778
XDOT = 2882
728121 Wp = 45
97288
YDOT = 4174
610785 meter/sec RA = 300
61598 deg
ZDOT = 5758
161904 TA = 330
04945
MA = 330
14843
Ha = 221
923 n
mi
Hp = 214
317
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14185748
34 X = 4372438
90
Y = -16442044
20 feet Y = -4962911
56 meter
Z = 4792868
88 Z = 1481987
53
XDOT = 9457
769426 XDOT = 2807
862054
YDOT = 13696
229610 feet/sec YDOT = 4206
428020 meter/sec
ZDOT = 18891
607297 ZDOT = 5771
983987
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19204730
11 X = -5853601
74
Y = 10091743
49 feet Y = 3075963
42 meter
Z = 4887015
49 Z = 1489562
32
XDOT = -2912
885788 XDOT = -887
847588
YDOT = -14768
767148 feet/sec YDOT = -4501
520227 meter/sec
ZDOT = 18951
842006 ZDOT = 5776
521443
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 17187
71279131
00016717 00000-0 10270-3 0 9091
2 25544 51
6411 301
0058 0005406 3
2745 356
8442 15
54103459 24783
Satellite: ISS
Catalog Number: 25544
Epoch time: 17187
71279131 = yrday
fracday
Element set: 909
Inclination: 51
6411 deg
RA of node: 301
0058 deg
Eccentricity:
0005406
Arg of perigee: 3
2745 deg
Mean anomaly: 356
8442 deg
Mean motion: 15
54103459 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2478
Checksum: 298
Coasting Arc #11 (Orbit 2492)
---------------------------------------
Vector Time (GMT): 2017/188/15:38:00
000
Vector Time (MET): N/A
Weight (LBS) : 901313
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4594092
70 A = 6785349
59 meter
Y = 3981557
09 meter E =
0006411
Z = -3023091
94 I = 51
31222
XDOT = -1657
649330 Wp = 51
35196
YDOT = -5639
372874 meter/sec RA = 295
61884 deg
ZDOT = -4911
397529 TA = 163
42840
MA = 163
40744
Ha = 222
040 n
mi
Hp = 214
041
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15072482
62 X = -4623589
48
Y = 13062851
34 feet Y = 3930018
33 meter
Z = -9918280
64 Z = -3045479
56
XDOT = -5438
482055 XDOT = -1570
608177
YDOT = -18501
879507 feet/sec YDOT = -5657
422467 meter/sec
ZDOT = -16113
508955 ZDOT = -4919
239208
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18639700
09 X = 5681380
59
Y = -6956646
25 feet Y = -2120385
78 meter
Z = -10017822
20 Z = -3053432
21
XDOT = -2015
187440 XDOT = -614
229132
YDOT = 17838
156200 feet/sec YDOT = 5437
070010 meter/sec
ZDOT = -16147
088381 ZDOT = -4921
632539
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 17188
67731900
00016717 00000-0 10270-3 0 9106
2 25544 51
6413 296
1979 0005425 7
8161 352
3075 15
54138550 24934
Satellite: ISS
Catalog Number: 25544
Epoch time: 17188
67731900 = yrday
fracday
Element set: 910
Inclination: 51
6413 deg
RA of node: 296
1979 deg
Eccentricity:
0005425
Arg of perigee: 7
8161 deg
Mean anomaly: 352
3075 deg
Mean motion: 15
54138550 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2493
Checksum: 314
Coasting Arc #12 (Orbit 2508)
---------------------------------------
Vector Time (GMT): 2017/189/15:38:00
000
Vector Time (MET): N/A
Weight (LBS) : 901313
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4605598
40 A = 6781511
35 meter
Y = -2587566
33 meter E =
0010777
Z = 4241573
07 I = 51
28546
XDOT = 511
262846 Wp = 76
79270
YDOT = 6773
201209 meter/sec RA = 290
61123 deg
ZDOT = 3571
593675 TA = 336
56603
MA = 336
61510
Ha = 221
947 n
mi
Hp = 214
002
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15110230
96 X = 4613587
67
Y = -8489390
86 feet Y = -2536019
33 meter
Z = 13915922
15 Z = 4263964
47
XDOT = 1677
371541 XDOT = 418
136248
YDOT = 22221
788745 feet/sec YDOT = 6778
397300 meter/sec
ZDOT = 11717
827019 ZDOT = 3573
851959
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16995151
44 X = -5180122
16
Y = 2963118
78 feet Y = 903158
61 meter
Z = 14015223
17 Z = 4271840
02
XDOT = 6156
622461 XDOT = 1876
538526
YDOT = -20234
547663 feet/sec YDOT = -6167
490128 meter/sec
ZDOT = 11726
569536 ZDOT = 3574
258395
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 17189
70614602
00016717 00000-0 10270-3 0 9111
2 25544 51
6404 291
0698 0005409 11
1107 349
0164 15
54150322 25097
Satellite: ISS
Catalog Number: 25544
Epoch time: 17189
70614602 = yrday
fracday
Element set: 911
Inclination: 51
6404 deg
RA of node: 291
0698 deg
Eccentricity:
0005409
Arg of perigee: 11
1107 deg
Mean anomaly: 349
0164 deg
Mean motion: 15
54150322 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2509
Checksum: 282
Coasting Arc #13 (Orbit 2521)
---------------------------------------
Vector Time (GMT): 2017/190/12:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 901313
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3307584
20 A = 6787537
26 meter
Y = 5577242
51 meter E =
0005482
Z = -2010897
42 I = 51
29743
XDOT = -3440
979826 Wp = 90
43734
YDOT = -4030
848645 meter/sec RA = 286
28276 deg
ZDOT = -5532
932223 TA = 111
86855
MA = 111
81024
Ha = 222
067 n
mi
Hp = 213
959
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10851654
20 X = -3359936
74
Y = 18298039
73 feet Y = 5539962
41 meter
Z = -6597432
47 Z = -2027090
86
XDOT = -11289
303892 XDOT = -3368
774135
YDOT = -13224
569045 feet/sec YDOT = -4068
923555 meter/sec
ZDOT = -18152
664773 ZDOT = -5549
472396
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21000870
33 X = 6401065
28
Y = 3252466
77 feet Y = 991351
87 meter
Z = -6669908
34 Z = -2032988
06
XDOT = -7903
761516 XDOT = -2409
066510
YDOT = 13747
111311 feet/sec YDOT = 4190
119528 meter/sec
ZDOT = -18224
952145 ZDOT = -5554
965414
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 17190
54206666
00016717 00000-0 10270-3 0 9123
2 25544 51
6416 286
9016 0005137 13
3149 346
8138 15
54140618 25223
Satellite: ISS
Catalog Number: 25544
Epoch time: 17190
54206666 = yrday
fracday
Element set: 912
Inclination: 51
6416 deg
RA of node: 286
9016 deg
Eccentricity:
0005137
Arg of perigee: 13
3149 deg
Mean anomaly: 346
8138 deg
Mean motion: 15
54140618 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2522
Checksum: 300
Coasting Arc #14 (Orbit 2537)
---------------------------------------
Vector Time (GMT): 2017/191/12:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 901313
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3721399
41 A = 6784070
04 meter
Y = -4483344
04 meter E =
0014582
Z = 3458052
22 I = 51
27842
XDOT = 2575
933188 Wp = 70
79280
YDOT = 5637
632278 meter/sec RA = 281
27992 deg
ZDOT = 4526
124311 TA = 330
06359
MA = 330
14690
Ha = 222
042 n
mi
Hp = 213
815
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12209315
66 X = 3754459
49
Y = -14709133
98 feet Y = -4441544
39 meter
Z = 11345315
68 Z = 3476209
12
XDOT = 8451
224369 XDOT = 2490
714880
YDOT = 18496
168892 feet/sec YDOT = 5665
961080 meter/sec
ZDOT = 14849
489210 ZDOT = 4538
430918
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18256730
03 X = -5564651
31
Y = -5502246
94 feet Y = -1677084
87 meter
Z = 11426254
26 Z = 3482722
30
XDOT = 13426
049944 XDOT = 4092
260023
YDOT = -13526
393541 feet/sec YDOT = -4122
844751 meter/sec
ZDOT = 14902
818559 ZDOT = 4542
379097
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 17191
57088689
00016717 00000-0 10270-3 0 9131
2 25544 51
6421 281
7729 0005283 16
9840 343
1489 15
54166057 25383
Satellite: ISS
Catalog Number: 25544
Epoch time: 17191
57088689 = yrday
fracday
Element set: 913
Inclination: 51
6421 deg
RA of node: 281
7729 deg
Eccentricity:
0005283
Arg of perigee: 16
9840 deg
Mean anomaly: 343
1489 deg
Mean motion: 15
54166057 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2538
Checksum: 338
Coasting Arc #15 (Orbit 2552)
---------------------------------------
Vector Time (GMT): 2017/192/12:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 901313
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4018482
44 A = 6780379
67 meter
Y = 3013804
43 meter E =
0014127
Z = -4568532
05 I = 51
25892
XDOT = -1687
407765 Wp = 53
15493
YDOT = -6830
468006 meter/sec RA = 276
26717 deg
ZDOT = -3019
920332 TA = 186
45923
MA = 186
47746
Ha = 222
266 n
mi
Hp = 213
633
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13183997
52 X = -4029693
60
Y = 9887809
80 feet Y = 2968804
82 meter
Z = -14988622
20 Z = -4588079
20
XDOT = -5536
114716 XDOT = -1596
233203
YDOT = -22409
671937 feet/sec YDOT = -6848
827640 meter/sec
ZDOT = -9907
875105 ZDOT = -3027
896379
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14317711
87 X = 4364038
58
Y = 7998737
37 feet Y = 2438015
15 meter
Z = -15075433
52 Z = -4594992
14
XDOT = -17728
835535 XDOT = -5403
749071
YDOT = 12985
659468 feet/sec YDOT = 3958
029006 meter/sec
ZDOT = -9941
898177 ZDOT = -3030
290564
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 17192
53540575
00016717 00000-0 10270-3 0 9146
2 25544 51
6407 276
9657 0005311 20
1239 340
0122 15
54136632 25537
Satellite: ISS
Catalog Number: 25544
Epoch time: 17192
53540575 = yrday
fracday
Element set: 914
Inclination: 51
6407 deg
RA of node: 276
9657 deg
Eccentricity:
0005311
Arg of perigee: 20
1239 deg
Mean anomaly: 340
0122 deg
Mean motion: 15
54136632 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2553
Checksum: 287
Coasting Arc #16 (Orbit 2568)
---------------------------------------
Vector Time (GMT): 2017/193/12:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 901313
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4181359
31 A = 6777680
84 meter
Y = -1277719
20 meter E =
0006045
Z = 5173661
35 I = 51
24778
XDOT = 807
472857 Wp = 64
27735
YDOT = 7534
234709 meter/sec RA = 271
24409 deg
ZDOT = 1209
575740 TA = 14
06946
MA = 14
05263
Ha = 222
111 n
mi
Hp = 213
614
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13718370
45 X = 4170205
63
Y = -4191992
13 feet Y = -1231023
22 meter
Z = 16973954
57 Z = 5193945
58
XDOT = 2649
189162 XDOT = 717
287614
YDOT = 24718
617811 feet/sec YDOT = 7542
760056 meter/sec
ZDOT = 3968
424345 ZDOT = 1213
279749
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9497360
85 X = -2894795
59
Y = -10607134
00 feet Y = -3233054
44 meter
Z = 17063717
78 Z = 5201021
18
XDOT = 20582
557284 XDOT = 6273
563460
YDOT = -12028
603492 feet/sec YDOT = -3666
318344 meter/sec
ZDOT = 3983
488655 ZDOT = 1214
167342
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 17193
56422171
00016717 00000-0 10270-3 0 9152
2 25544 51
6407 271
8371 0005327 23
3286 336
8107 15
54179487 25696
Satellite: ISS
Catalog Number: 25544
Epoch time: 17193
56422171 = yrday
fracday
Element set: 915
Inclination: 51
6407 deg
RA of node: 271
8371 deg
Eccentricity:
0005327
Arg of perigee: 23
3286 deg
Mean anomaly: 336
8107 deg
Mean motion: 15
54179487 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2569
Checksum: 322
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