[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
June 9th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 8611 13 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 126 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 637 ET - UTC (sec) : 67 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
162/10:20:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
6
000/00:00:00
000 0
0 0
0 212
0
Coasting Arc #1 (Orbit 2674)
---------------------------------------
Vector Time (GMT): 2015/159/20:34:59
332
Vector Time (MET): N/A
Weight (LBS) : 892082
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5147089
11 A = 6780155
72 meter
Y = 2181805
63 meter E =
0013169
Z = 3823098
00 I = 51
93703
XDOT = 419
281488 Wp = 78
72250
YDOT = -6404
731267 meter/sec RA = 124
65011 deg
ZDOT = 4209
882640 TA = 327
08192
MA = 327
16386
Ha = 220
450 n
mi
Hp = 212
338
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16886775
28 X = -5189675
21
Y = 7158154
96 feet Y = 2124009
12 meter
Z = 12542972
43 Z = 3797991
16
XDOT = 1375
595432 XDOT = 470
419535
YDOT = -21012
897857 feet/sec YDOT = -6399
756969 meter/sec
ZDOT = 13811
950917 ZDOT = 4212
043163
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12394724
13 X = 3777911
92
Y = -13619055
81 feet Y = -4151088
21 meter
Z = 12434655
28 Z = 3790082
93
XDOT = 6656
779670 XDOT = 2028
986443
YDOT = 18708
018922 feet/sec YDOT = 5702
204168 meter/sec
ZDOT = 13822
383664 ZDOT = 4213
062541
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 15159
91377487
00016717 00000-0 10270-3 0 9004
2 25544 51
6410 125
3495 0004317 20
4475 339
6851 15
55183597 26759
Satellite: ISS
Catalog Number: 25544
Epoch time: 15159
91377487 = yrday
fracday
Element set: 900
Inclination: 51
6410 deg
RA of node: 125
3495 deg
Eccentricity:
0004317
Arg of perigee: 20
4475 deg
Mean anomaly: 339
6851 deg
Mean motion: 15
55183597 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2675
Checksum: 327
Coasting Arc #2 (Orbit 2689)
---------------------------------------
Vector Time (GMT): 2015/160/20:34:59
332
Vector Time (MET): N/A
Weight (LBS) : 892082
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4621890
99 A = 6775922
86 meter
Y = -263811
99 meter E =
0015505
Z = -4962189
07 I = 51
93931
XDOT = -1999
683126 Wp = 62
09051
YDOT = 7046
213218 meter/sec RA = 119
66936 deg
ZDOT = -2235
417274 TA = 186
13863
MA = 186
15765
Ha = 220
395 n
mi
Hp = 212
295
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15163684
34 X = 4648602
01
Y = -865524
90 feet Y = -211977
31 meter
Z = -16280147
87 Z = -4939671
89
XDOT = -6560
640177 XDOT = -2067
468095
YDOT = 23117
497434 feet/sec YDOT = 7023
472590 meter/sec
ZDOT = -7334
046173 ZDOT = -2245
295560
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13367511
01 X = -4074417
36
Y = 7425642
05 feet Y = 2263335
70 meter
Z = -16183298
81 Z = -4932669
48
XDOT = -3655
813294 XDOT = -1114
291892
YDOT = -22672
634194 feet/sec YDOT = -6910
618902 meter/sec
ZDOT = -7377
782032 ZDOT = -2248
747963
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 15160
87764759
00016717 00000-0 10270-3 0 9014
2 25544 51
6399 120
5361 0004305 26
5942 333
5432 15
55198373 26900
Satellite: ISS
Catalog Number: 25544
Epoch time: 15160
87764759 = yrday
fracday
Element set: 901
Inclination: 51
6399 deg
RA of node: 120
5361 deg
Eccentricity:
0004305
Arg of perigee: 26
5942 deg
Mean anomaly: 333
5432 deg
Mean motion: 15
55198373 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2690
Checksum: 318
Coasting Arc #3 (Orbit 2705)
---------------------------------------
Vector Time (GMT): 2015/161/20:34:59
332
Vector Time (MET): N/A
Weight (LBS) : 892082
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3757288
04 A = 6774295
63 meter
Y = -1818125
80 meter E =
0005959
Z = 5331643
22 I = 51
94868
XDOT = 3255
239360 Wp = 50
64391
YDOT = -6949
252601 meter/sec RA = 114
67909 deg
ZDOT = -71
989442 TA = 40
06061
MA = 40
01668
Ha = 220
615 n
mi
Hp = 212
107
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12327060
51 X = -3762577
37
Y = -5964979
65 feet Y = -1860172
18 meter
Z = 17492267
79 Z = 5313377
95
XDOT = 10679
919160 XDOT = 3333
055327
YDOT = -22799
385175 feet/sec YDOT = -6912
415285 meter/sec
ZDOT = -236
185834 ZDOT = -55
987475
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13790842
51 X = 4203448
80
Y = -282184
24 feet Y = -86009
76 meter
Z = 17414071
05 Z = 5307808
86
XDOT = 719
693297 XDOT = 219
362517
YDOT = 24160
857888 feet/sec YDOT = 7364
229484 meter/sec
ZDOT = -166
126039 ZDOT = -50
635217
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 15161
90576808
00016717 00000-0 10270-3 0 9026
2 25544 51
6399 115
4014 0004291 30
8581 329
2824 15
55176137 27068
Satellite: ISS
Catalog Number: 25544
Epoch time: 15161
90576808 = yrday
fracday
Element set: 902
Inclination: 51
6399 deg
RA of node: 115
4014 deg
Eccentricity:
0004291
Arg of perigee: 30
8581 deg
Mean anomaly: 329
2824 deg
Mean motion: 15
55176137 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2706
Checksum: 308
Coasting Arc #4 (Orbit 2714)
---------------------------------------
Vector Time (GMT): 2015/162/10:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 876851
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4611737
85 A = 6777053
77 meter
Y = 1752245
33 meter E =
0009924
Z = 4637894
81 I = 51
96604
XDOT = 320
256121 Wp = 89
17492
YDOT = -7065
461328 meter/sec RA = 111
85583 deg
ZDOT = 2982
508890 TA = 331
23904
MA = 331
29372
Ha = 220
562 n
mi
Hp = 211
972
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15130373
53 X = -4653518
47
Y = 5748836
38 feet Y = 1700439
91 meter
Z = 15216190
33 Z = 4615390
34
XDOT = 1050
709059 XDOT = 384
751964
YDOT = -23180
647403 feet/sec YDOT = -7061
519617 meter/sec
ZDOT = 9785
134153 ZDOT = 2984
220781
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4406251
17 X = -1343025
36
Y = 15668666
51 feet Y = 4775809
55 meter
Z = 15119114
10 Z = 4608305
98
XDOT = -16929
290179 XDOT = -5160
047647
YDOT = -14228
076376 feet/sec YDOT = -4336
717680 meter/sec
ZDOT = 9793
786348 ZDOT = 2985
146079
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 15162
48407928
00016717 00000-0 10270-3 0 9037
2 25544 51
6401 112
5158 0004328 32
1000 328
0416 15
55242805 27151
Satellite: ISS
Catalog Number: 25544
Epoch time: 15162
48407928 = yrday
fracday
Element set: 903
Inclination: 51
6401 deg
RA of node: 112
5158 deg
Eccentricity:
0004328
Arg of perigee: 32
1000 deg
Mean anomaly: 328
0416 deg
Mean motion: 15
55242805 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2715
Checksum: 272
Coasting Arc #5 (Orbit 2729)
---------------------------------------
Vector Time (GMT): 2015/163/10:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 876851
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4212773
88 A = 6774349
95 meter
Y = 406176
28 meter E =
0017884
Z = -5304860
21 I = 51
96812
XDOT = -1651
853418 Wp = 73
72921
YDOT = 7440
236486 meter/sec RA = 106
86906 deg
ZDOT = -739
309035 TA = 189
21341
MA = 189
24627
Ha = 220
541 n
mi
Hp = 212
001
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13821436
62 X = 4233688
12
Y = 1332599
35 feet Y = 453403
69 meter
Z = -17404397
00 Z = -5284344
31
XDOT = -5419
466595 XDOT = -1731
337828
YDOT = 24410
224692 feet/sec YDOT = 7421
320024 meter/sec
ZDOT = -2425
554576 ZDOT = -747
525898
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9157154
00 X = 2791100
54
Y = -10583695
00 feet Y = -3225910
23 meter
Z = -17316261
06 Z = -5277996
37
XDOT = 15991
982321 XDOT = 4874
356211
YDOT = 17880
206680 feet/sec YDOT = 5449
886996 meter/sec
ZDOT = -2462
261287 ZDOT = -750
497240
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 15163
44792575
00016717 00000-0 10270-3 0 9040
2 25544 51
6404 107
7018 0004444 36
5209 323
6246 15
55227312 27308
Satellite: ISS
Catalog Number: 25544
Epoch time: 15163
44792575 = yrday
fracday
Element set: 904
Inclination: 51
6404 deg
RA of node: 107
7018 deg
Eccentricity:
0004444
Arg of perigee: 36
5209 deg
Mean anomaly: 323
6246 deg
Mean motion: 15
55227312 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2730
Checksum: 292
Coasting Arc #6 (Orbit 2745)
---------------------------------------
Vector Time (GMT): 2015/164/10:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 876851
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3555167
53 A = 6774934
71 meter
Y = -2612078
82 meter E =
0009311
Z = 5137360
16 I = 51
97917
XDOT = 2764
370175 Wp = 47
43660
YDOT = -6972
314892 meter/sec RA = 101
88017 deg
ZDOT = -1624
051474 TA = 58
19172
MA = 58
10108
Ha = 220
645 n
mi
Hp = 211
789
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11663935
46 X = -3550650
05
Y = -8569812
40 feet Y = -2651810
33 meter
Z = 16854856
18 Z = 5120100
34
XDOT = 9069
455954 XDOT = 2850
019933
YDOT = -22875
048858 feet/sec YDOT = -6940
922823 meter/sec
ZDOT = -5328
252866 ZDOT = -1610
415272
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13721981
53 X = -4182459
97
Y = 4865814
01 feet Y = 1483100
11 meter
Z = 16781130
14 Z = 5114888
47
XDOT = -13368
549923 XDOT = -4074
734017
YDOT = -19440
198385 feet/sec YDOT = -5925
372468 meter/sec
ZDOT = -5268
311010 ZDOT = -1605
781196
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 15164
47601656
00016717 00000-0 10270-3 0 9054
2 25544 51
6408 102
5680 0004449 39
0721 321
0753 15
55251517 27468
Satellite: ISS
Catalog Number: 25544
Epoch time: 15164
47601656 = yrday
fracday
Element set: 905
Inclination: 51
6408 deg
RA of node: 102
5680 deg
Eccentricity:
0004449
Arg of perigee: 39
0721 deg
Mean anomaly: 321
0753 deg
Mean motion: 15
55251517 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2746
Checksum: 296
Coasting Arc #7 (Orbit 2760)
---------------------------------------
Vector Time (GMT): 2015/165/10:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 876851
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2760819
05 A = 6778613
81 meter
Y = 4549474
03 meter E =
0010398
Z = -4207253
54 I = 51
99770
XDOT = -3615
795611 Wp = 86
28116
YDOT = 5633
827784 meter/sec RA = 96
89940 deg
ZDOT = 3727
956118 TA = 221
80804
MA = 221
88752
Ha = 220
601 n
mi
Hp = 211
785
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9057805
30 X = 2730178
01
Y = 14926095
91 feet Y = 4580176
53 meter
Z = -13803325
28 Z = -4193915
74
XDOT = -11862
846492 XDOT = -3696
634871
YDOT = 18483
686954 feet/sec YDOT = 5592
941122 meter/sec
ZDOT = 12230
827159 ZDOT = 3710
195473
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17493926
48 X = 5332148
79
Y = 592500
77 feet Y = 180594
24 meter
Z = -13746833
96 Z = -4190034
99
XDOT = 8888
764041 XDOT = 2709
295280
YDOT = 18874
219519 feet/sec YDOT = 5752
862109 meter/sec
ZDOT = 12153
382373 ZDOT = 3704
350947
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 15165
43984081
00016717 00000-0 10270-3 0 9068
2 25544 51
6414 97
7549 0004473 41
6516 318
4978 15
55253767 27617
Satellite: ISS
Catalog Number: 25544
Epoch time: 15165
43984081 = yrday
fracday
Element set: 906
Inclination: 51
6414 deg
RA of node: 97
7549 deg
Eccentricity:
0004473
Arg of perigee: 41
6516 deg
Mean anomaly: 318
4978 deg
Mean motion: 15
55253767 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2761
Checksum: 339
Coasting Arc #8 (Orbit 2776)
---------------------------------------
Vector Time (GMT): 2015/166/10:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 876851
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1818716
71 A = 6783131
93 meter
Y = -5994755
76 meter E =
0016450
Z = 2586978
64 I = 52
01700
XDOT = 4250
970140 Wp = 90
05433
YDOT = -3583
434574 meter/sec RA = 91
93342 deg
ZDOT = -5286
384669 TA = 60
98176
MA = 60
81701
Ha = 220
579 n
mi
Hp = 211
614
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5966918
34 X = -1764113
40
Y = -19667833
87 feet Y = -6014788
90 meter
Z = 8487462
74 Z = 2578275
40
XDOT = 13946
752427 XDOT = 4316
404463
YDOT = -11756
675113 feet/sec YDOT = -3535
530843 meter/sec
ZDOT = -17343
781723 ZDOT = -5265
575706
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19826496
28 X = -6043116
07
Y = -5472870
94 feet Y = -1668131
06 meter
Z = 8451186
68 Z = 2575921
70
XDOT = -2778
202387 XDOT = -846
796087
YDOT = -16725
389681 feet/sec YDOT = -5097
898775 meter/sec
ZDOT = -17253
602933 ZDOT = -5258
898174
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 15166
46790926
00016717 00000-0 10270-3 0 9076
2 25544 51
6423 92
6208 0004493 45
1656 314
9862 15
55293106 27770
Satellite: ISS
Catalog Number: 25544
Epoch time: 15166
46790926 = yrday
fracday
Element set: 907
Inclination: 51
6423 deg
RA of node: 92
6208 deg
Eccentricity:
0004493
Arg of perigee: 45
1656 deg
Mean anomaly: 314
9862 deg
Mean motion: 15
55293106 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2777
Checksum: 330
Coasting Arc #9 (Orbit 2791)
---------------------------------------
Vector Time (GMT): 2015/167/10:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 876851
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 825192
19 A = 6785752
04 meter
Y = 6701506
91 meter E =
0015222
Z = -603497
30 I = 52
02623
XDOT = -4639
221864 Wp = 43
03346
YDOT = 1103
478186 meter/sec RA = 86
98067 deg
ZDOT = 6009
754129 TA = 310
48214
MA = 310
61471
Ha = 220
575 n
mi
Hp = 211
535
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2707323
47 X = 753124
58
Y = 21986571
24 feet Y = 6710331
89 meter
Z = -1979978
02 Z = -599662
72
XDOT = -15220
544174 XDOT = -4680
409637
YDOT = 3620
335257 feet/sec YDOT = 1051
368194 meter/sec
ZDOT = 19717
041105 ZDOT = 5987
117742
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20172852
21 X = 6148685
35
Y = 9157230
38 feet Y = 2791123
82 meter
Z = -1964788
48 Z = -598867
53
XDOT = -4253
331047 XDOT = -1296
415303
YDOT = 13508
718010 feet/sec YDOT = 4117
457249 meter/sec
ZDOT = 19619
470629 ZDOT = 5980
014648
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 15167
43171259
00016717 00000-0 10270-3 0 9087
2 25544 51
6424 87
8081 0004446 48
4303 311
7230 15
55307112 27923
Satellite: ISS
Catalog Number: 25544
Epoch time: 15167
43171259 = yrday
fracday
Element set: 908
Inclination: 51
6424 deg
RA of node: 87
8081 deg
Eccentricity:
0004446
Arg of perigee: 48
4303 deg
Mean anomaly: 311
7230 deg
Mean motion: 15
55307112 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2792
Checksum: 294
Coasting Arc #10 (Orbit 2807)
---------------------------------------
Vector Time (GMT): 2015/168/10:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 876851
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 279324
02 A = 6784854
45 meter
Y = -6604056
41 meter E =
0009266
Z = -1527143
69 I = 52
02200
XDOT = 4780
803099 Wp = 113
61062
YDOT = 1534
412622 meter/sec RA = 82
03103 deg
ZDOT = -5792
364962 TA = 82
98285
MA = 82
87748
Ha = 220
558 n
mi
Hp = 211
474
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 916417
38 X = 360569
68
Y = -21666851
75 feet Y = -6600478
33 meter
Z = -5010313
94 Z = -1525590
43
XDOT = 15685
049537 XDOT = 4791
426715
YDOT = 5034
162146 feet/sec YDOT = 1587
934948 meter/sec
ZDOT = -19003
822054 ZDOT = -5769
114737
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18191714
26 X = -5544834
51
Y = -11808203
93 feet Y = -3599140
56 meter
Z = -5002337
78 Z = -1524712
56
XDOT = 11493
381724 XDOT = 3503
182750
YDOT = -9741
891678 feet/sec YDOT = -2969
328584 meter/sec
ZDOT = -18904
120113 ZDOT = -5761
975810
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 15168
45975860
00016717 00000-0 10270-3 0 9091
2 25544 51
6436 82
6739 0004449 51
3442 308
8109 15
55327166 28080
Satellite: ISS
Catalog Number: 25544
Epoch time: 15168
45975860 = yrday
fracday
Element set: 909
Inclination: 51
6436 deg
RA of node: 82
6739 deg
Eccentricity:
0004449
Arg of perigee: 51
3442 deg
Mean anomaly: 308
8109 deg
Mean motion: 15
55327166 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2808
Checksum: 335
Coasting Arc #11 (Orbit 2823)
---------------------------------------
Vector Time (GMT): 2015/169/10:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 876851
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1398443
88 A = 6780980
24 meter
Y = 5701331
70 meter E =
0016358
Z = 3377520
79 I = 52
00382
XDOT = -4651
346822 Wp = 80
46495
YDOT = -3923
117932 meter/sec RA = 77
07297 deg
ZDOT = 4679
880150 TA = 318
79417
MA = 318
91755
Ha = 220
609 n
mi
Hp = 211
388
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4588070
48 X = -1478500
26
Y = 18705156
49 feet Y = 5685245
28 meter
Z = 11081104
95 Z = 3370533
81
XDOT = -15260
324219 XDOT = -4629
864881
YDOT = -12871
121823 feet/sec YDOT = -3975
012885 meter/sec
ZDOT = 15353
937501 ZDOT = 4657
336528
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13988039
22 X = 4263554
35
Y = 13264919
52 feet Y = 4043147
47 meter
Z = 11049924
24 Z = 3368016
91
XDOT = -17795
907865 XDOT = -5424
192717
YDOT = 6010
638260 feet/sec YDOT = 1832
042542 meter/sec
ZDOT = 15257
743733 ZDOT = 4650
560290
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 15169
48779306
00016717 00000-0 10270-3 0 9104
2 25544 51
6435 77
5402 0004428 55
2887 304
8683 15
55342983 28247
Satellite: ISS
Catalog Number: 25544
Epoch time: 15169
48779306 = yrday
fracday
Element set: 910
Inclination: 51
6435 deg
RA of node: 77
5402 deg
Eccentricity:
0004428
Arg of perigee: 55
2887 deg
Mean anomaly: 304
8683 deg
Mean motion: 15
55342983 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2824
Checksum: 335
Coasting Arc #12 (Orbit 2838)
---------------------------------------
Vector Time (GMT): 2015/170/10:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 876851
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2554555
56 A = 6776291
05 meter
Y = -4136195
21 meter E =
0015284
Z = -4735426
95 I = 51
98081
XDOT = 4168
965247 Wp = 66
94769
YDOT = 5780
597071 meter/sec RA = 72
09840 deg
ZDOT = -2801
483012 TA = 175
39031
MA = 175
37622
Ha = 220
555 n
mi
Hp = 211
359
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8381087
78 X = 2623620
39
Y = -13570194
27 feet Y = -4107241
73 meter
Z = -15536177
65 Z = -4722850
28
XDOT = 13677
707504 XDOT = 4117
623842
YDOT = 18965
213486 feet/sec YDOT = 5826
930461 meter/sec
ZDOT = -9191
217230 ZDOT = -2781
355081
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7878290
14 X = -2401302
83
Y = -13929425
73 feet Y = -4245688
96 meter
Z = -15481255
25 Z = -4718686
60
XDOT = 22205
207318 XDOT = 6768
147190
YDOT = -2443
668423 feet/sec YDOT = -744
830135 meter/sec
ZDOT = -9105
785370 ZDOT = -2775
443381
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 15170
45156494
00016717 00000-0 10270-3 0 9111
2 25544 51
6439 72
7266 0004480 58
0459 302
1130 15
55371785 28396
Satellite: ISS
Catalog Number: 25544
Epoch time: 15170
45156494 = yrday
fracday
Element set: 911
Inclination: 51
6439 deg
RA of node: 72
7266 deg
Eccentricity:
0004480
Arg of perigee: 58
0459 deg
Mean anomaly: 302
1130 deg
Mean motion: 15
55371785 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2839
Checksum: 311
Coasting Arc #13 (Orbit 2854)
---------------------------------------
Vector Time (GMT): 2015/171/10:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 876851
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3615338
36 A = 6773679
59 meter
Y = 2125393
06 meter E =
0006386
Z = 5313802
73 I = 51
96163
XDOT = -3331
101120 Wp = 79
37135
YDOT = -6897
881730 meter/sec RA = 67
11108 deg
ZDOT = 493
260938 TA = 5
95245
MA = 5
94486
Ha = 220
584 n
mi
Hp = 211
249
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11861346
33 X = -3664648
57
Y = 6973074
35 feet Y = 2084687
68 meter
Z = 17433735
99 Z = 5296120
72
XDOT = -10928
809450 XDOT = -3256
115839
YDOT = -22630
845571 feet/sec YDOT = -6934
713071 meter/sec
ZDOT = 1618
310165 ZDOT = 477
260577
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 652595
63 X = 198911
15
Y = 13840177
00 feet Y = 4218485
95 meter
Z = 17357248
42 Z = 5290489
32
XDOT = -24115
125228 XDOT = -7350
290170
YDOT = -805
210327 feet/sec YDOT = -245
428108 meter/sec
ZDOT = 1550
861950 ZDOT = 472
702722
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 15171
47957593
00016717 00000-0 10270-3 0 9124
2 25544 51
6437 67
5926 0004285 60
8042 299
3540 15
55412088 28553
Satellite: ISS
Catalog Number: 25544
Epoch time: 15171
47957593 = yrday
fracday
Element set: 912
Inclination: 51
6437 deg
RA of node: 67
5926 deg
Eccentricity:
0004285
Arg of perigee: 60
8042 deg
Mean anomaly: 299
3540 deg
Mean motion: 15
55412088 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2855
Checksum: 331
Coasting Arc #14 (Orbit 2869)
---------------------------------------
Vector Time (GMT): 2015/172/10:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 876851
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4506806
24 A = 6774890
26 meter
Y = 28837
08 meter E =
0016604
Z = -5072956
66 I = 51
95263
XDOT = 2086
183073 Wp = 94
15231
YDOT = 7119
783061 meter/sec RA = 62
11932 deg
ZDOT = 1898
003646 TA = 194
16839
MA = 194
21501
Ha = 220
556 n
mi
Hp = 211
335
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14786109
71 X = 4530791
16
Y = 94609
85 feet Y = 79369
74 meter
Z = -16643558
59 Z = -5051005
37
XDOT = 6844
432655 XDOT = 1997
193184
YDOT = 23358
868312 feet/sec YDOT = 7142
614371 meter/sec
ZDOT = 6227
046084 ZDOT = 1907
922386
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6736999
04 X = 2053437
31
Y = -13280999
98 feet Y = -4048048
80 meter
Z = -16549136
46 Z = -5044176
79
XDOT = 22969
979798 XDOT = 7001
249842
YDOT = 3858
277720 feet/sec YDOT = 1176
003049 meter/sec
ZDOT = 6268
281179 ZDOT = 1910
572103
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 15172
44332856
00016717 00000-0 10270-3 0 9132
2 25544 51
6441 62
7786 0004409 64
0438 296
1169 15
55390712 28700
Satellite: ISS
Catalog Number: 25544
Epoch time: 15172
44332856 = yrday
fracday
Element set: 913
Inclination: 51
6441 deg
RA of node: 62
7786 deg
Eccentricity:
0004409
Arg of perigee: 64
0438 deg
Mean anomaly: 296
1169 deg
Mean motion: 15
55390712 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2870
Checksum: 316
Coasting Arc #15 (Orbit 2885)
---------------------------------------
Vector Time (GMT): 2015/173/10:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 876851
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5062514
16 A = 6778980
56 meter
Y = -2086412
35 meter E =
0015379
Z = 3986518
94 I = 51
95047
XDOT = -480
423042 Wp = 76
08420
YDOT = -6526
580516 meter/sec RA = 57
13644 deg
ZDOT = -4009
367974 TA = 55
54769
MA = 55
40246
Ha = 220
664 n
mi
Hp = 211
169
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16609298
41 X = -5058172
03
Y = -6845184
86 feet Y = -2143000
76 meter
Z = 13079130
38 Z = 3961936
75
XDOT = -1576
191084 XDOT = -387
929663
YDOT = -21412
665734 feet/sec YDOT = -6531
435418 meter/sec
ZDOT = -13154
094402 ZDOT = -4011
477662
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13374749
34 X = -4076623
60
Y = 12107245
09 feet Y = 3690288
30 meter
Z = 12973808
13 Z = 3954416
72
XDOT = -19080
155037 XDOT = -5815
631255
YDOT = -6915
199606 feet/sec YDOT = -2107
752840 meter/sec
ZDOT = -13161
849252 ZDOT = -4011
731652
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 15173
47131954
00016717 00000-0 10270-3 0 9143
2 25544 51
6438 57
6441 0004431 68
0485 292
1139 15
55402392 28866
Satellite: ISS
Catalog Number: 25544
Epoch time: 15173
47131954 = yrday
fracday
Element set: 914
Inclination: 51
6438 deg
RA of node: 57
6441 deg
Eccentricity:
0004431
Arg of perigee: 68
0485 deg
Mean anomaly: 292
1139 deg
Mean motion: 15
55402392 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2886
Checksum: 313
Coasting Arc #16 (Orbit 2900)
---------------------------------------
Vector Time (GMT): 2015/174/10:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 876851
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5174668
20 A = 6783355
37 meter
Y = 3736443
76 meter E =
0010036
Z = -2293492
19 I = 51
94827
XDOT = -1357
013631 Wp = 54
89888
YDOT = 5213
874238 meter/sec RA = 52
16737 deg
ZDOT = 5454
863091 TA = 279
66920
MA = 279
78255
Ha = 220
536 n
mi
Hp = 211
140
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16977257
89 X = 5143642
68
Y = 12258673
75 feet Y = 3794136
99 meter
Z = -7524580
68 Z = -2268429
82
XDOT = -4452
144460 XDOT = -1441
713141
YDOT = 17105
886607 feet/sec YDOT = 5198
225211 meter/sec
ZDOT = 17896
532451 ZDOT = 5448
065692
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18226674
00 X = 5555490
24
Y = -10387022
39 feet Y = -3165964
43 meter
Z = -7417533
44 Z = -2260864
19
XDOT = 12902
980217 XDOT = 3932
828370
YDOT = 9936
308997 feet/sec YDOT = 3028
586982 meter/sec
ZDOT = 17866
232051 ZDOT = 5445
627529
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 15174
43505012
00016717 00000-0 10270-3 0 9151
2 25544 51
6446 52
8301 0004352 70
9135 289
2489 15
55435786 29019
Satellite: ISS
Catalog Number: 25544
Epoch time: 15174
43505012 = yrday
fracday
Element set: 915
Inclination: 51
6446 deg
RA of node: 52
8301 deg
Eccentricity:
0004352
Arg of perigee: 70
9135 deg
Mean anomaly: 289
2489 deg
Mean motion: 15
55435786 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2901
Checksum: 304
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