[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
April 6th 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14929 5432 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 102 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 3 055 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
104/12:22:23
007 1
8 1
8 1
8
N/A 0
3 -0
2 221
3
000/00:04:42
014 -0
1 -0
0 214
4
109/04:50:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
3
000/00:00:00
000 0
0 0
0 214
0
Coasting Arc #1 (Orbit 3382)
---------------------------------------
Vector Time (GMT): 2016/097/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922442
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -912553
37 A = 6783863
43 meter
Y = -5841303
62 meter E =
0006422
Z = -3334191
74 I = 51
94936
XDOT = 5766
309620 Wp = 71
52236
YDOT = 1788
235742 meter/sec RA = 54
92668 deg
ZDOT = -4716
541861 TA = 147
07204
MA = 147
03202
Ha = 221
247 n
mi
Hp = 213
728
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2993941
50 X = -830970
45
Y = -19164381
97 feet Y = -5851052
72 meter
Z = -10938949
28 Z = -3338425
74
XDOT = 18918
338647 XDOT = 5768
795655
YDOT = 5866
915163 feet/sec YDOT = 1852
731683 meter/sec
ZDOT = -15474
218704 ZDOT = -4688
524590
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7584505
08 X = -2311757
15
Y = -17841901
53 feet Y = -5438211
59 meter
Z = -10956261
49 Z = -3339468
50
XDOT = 18576
909377 XDOT = 5662
241978
YDOT = 1519
841159 feet/sec YDOT = 463
247585 meter/sec
ZDOT = -15352
774397 ZDOT = -4679
525636
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 16097
52524046
00016717 00000-0 10270-3 0 9008
2 25544 51
6408 55
4611 0002672 31
1341 328
9970 15
54382807 33836
Satellite: ISS
Catalog Number: 25544
Epoch time: 16097
52524046 = yrday
fracday
Element set: 900
Inclination: 51
6408 deg
RA of node: 55
4611 deg
Eccentricity:
0002672
Arg of perigee: 31
1341 deg
Mean anomaly: 328
9970 deg
Mean motion: 15
54382807 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3383
Checksum: 298
Coasting Arc #2 (Orbit 3398)
---------------------------------------
Vector Time (GMT): 2016/098/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922442
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -397488
62 A = 6779807
29 meter
Y = 5031567
82 meter E =
0009636
Z = 4519178
73 I = 51
91728
XDOT = -6106
727407 Wp = 97
66833
YDOT = -3365
674529 meter/sec RA = 49
95914 deg
ZDOT = 3203
075165 TA = 320
26889
MA = 320
33943
Ha = 221
188 n
mi
Hp = 213
679
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1304096
53 X = -475675
81
Y = 16507768
44 feet Y = 5026686
27 meter
Z = 14826701
89 Z = 4517057
23
XDOT = -20035
194905 XDOT = -6084
197076
YDOT = -11042
239269 feet/sec YDOT = -3433
837617 meter/sec
ZDOT = 10508
776788 ZDOT = 3173
465036
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3018584
59 X = 920064
58
Y = 16291000
59 feet Y = 4965496
98 meter
Z = 14816532
05 Z = 4516078
97
XDOT = -21119
381355 XDOT = -6437
187437
YDOT = -5549
075098 feet/sec YDOT = -1691
358090 meter/sec
ZDOT = 10380
716906 ZDOT = 3164
042513
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 16098
55390452
00016717 00000-0 10270-3 0 9015
2 25544 51
6411 50
3324 0002449 33
7122 326
4186 15
54422753 33996
Satellite: ISS
Catalog Number: 25544
Epoch time: 16098
55390452 = yrday
fracday
Element set: 901
Inclination: 51
6411 deg
RA of node: 50
3324 deg
Eccentricity:
0002449
Arg of perigee: 33
7122 deg
Mean anomaly: 326
4186 deg
Mean motion: 15
54422753 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3399
Checksum: 295
Coasting Arc #3 (Orbit 3413)
---------------------------------------
Vector Time (GMT): 2016/099/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922442
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1851126
04 A = 6777093
57 meter
Y = -3932380
21 meter E =
0015995
Z = -5213964
72 I = 51
88750
XDOT = 6010
991498 Wp = 73
65685
YDOT = 4560
218122 meter/sec RA = 44
97853 deg
ZDOT = -1304
159148 TA = 183
83482
MA = 183
84709
Ha = 221
242 n
mi
Hp = 213
705
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6073248
18 X = 1920288
89
Y = -12901509
89 feet Y = -3911293
57 meter
Z = -17106183
47 Z = -5204803
85
XDOT = 19721
100714 XDOT = 5965
886390
YDOT = 14961
345543 feet/sec YDOT = 4627
184681 meter/sec
ZDOT = -4278
737362 ZDOT = -1275
068898
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2306205
89 X = 702931
56
Y = -14120936
93 feet Y = -4304061
58 meter
Z = -17065619
48 Z = -5201600
82
XDOT = 22128
091027 XDOT = 6744
642145
YDOT = 8637
417919 feet/sec YDOT = 2632
684982 meter/sec
ZDOT = -4153
178130 ZDOT = -1265
888694
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 16099
51827112
00016717 00000-0 10270-3 0 9021
2 25544 51
6421 45
5229 0002557 36
8395 323
2934 15
54401982 34148
Satellite: ISS
Catalog Number: 25544
Epoch time: 16099
51827112 = yrday
fracday
Element set: 902
Inclination: 51
6421 deg
RA of node: 45
5229 deg
Eccentricity:
0002557
Arg of perigee: 36
8395 deg
Mean anomaly: 323
2934 deg
Mean motion: 15
54401982 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3414
Checksum: 303
Coasting Arc #4 (Orbit 3429)
---------------------------------------
Vector Time (GMT): 2016/100/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922442
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3309906
45 A = 6776678
45 meter
Y = 2641624
85 meter E =
0005723
Z = 5287102
07 I = 51
86346
XDOT = -5457
693868 Wp = 50
70828
YDOT = -5340
958559 meter/sec RA = 39
99293 deg
ZDOT = -744
096826 TA = 46
39826
MA = 46
35078
Ha = 221
373 n
mi
Hp = 213
562
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10859273
13 X = -3364882
62
Y = 8666748
18 feet Y = 2604304
35 meter
Z = 17346135
39 Z = 5270889
36
XDOT = -17905
819776 XDOT = -5393
949751
YDOT = -17522
829918 feet/sec YDOT = -5401
633773 meter/sec
ZDOT = -2441
262554 ZDOT = -770
454042
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7893789
20 X = -2406026
95
Y = 11540427
04 feet Y = 3517522
16 meter
Z = 17275166
73 Z = 5265470
82
XDOT = -21452
545263 XDOT = -6538
735796
YDOT = -10829
397708 feet/sec YDOT = -3300
800421 meter/sec
ZDOT = -2554
779025 ZDOT = -778
696647
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 16100
54691612
00016717 00000-0 10270-3 0 9032
2 25544 51
6425 40
3941 0002648 38
7546 321
3796 15
54426312 34303
Satellite: ISS
Catalog Number: 25544
Epoch time: 16100
54691612 = yrday
fracday
Element set: 903
Inclination: 51
6425 deg
RA of node: 40
3941 deg
Eccentricity:
0002648
Arg of perigee: 38
7546 deg
Mean anomaly: 321
3796 deg
Mean motion: 15
54426312 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3430
Checksum: 289
Coasting Arc #5 (Orbit 3444)
---------------------------------------
Vector Time (GMT): 2016/101/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 944180
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4641551
92 A = 6778931
40 meter
Y = -1325131
85 meter E =
0012344
Z = -4770856
04 I = 51
84539
XDOT = 4389
499129 Wp = 97
34719
YDOT = 5665
518381 meter/sec RA = 35
00770 deg
ZDOT = 2701
347202 TA = 199
27834
MA = 199
32509
Ha = 221
303 n
mi
Hp = 213
618
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15228188
71 X = 4679199
99
Y = -4347545
43 feet Y = -1273016
74 meter
Z = -15652414
84 Z = -4748216
70
XDOT = 14401
243861 XDOT = 4312
697489
YDOT = 18587
658731 feet/sec YDOT = 5714
175435 meter/sec
ZDOT = 8862
687671 ZDOT = 2722
483664
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13187861
50 X = 4019660
18
Y = -8941896
07 feet Y = -2725489
92 meter
Z = -15553770
50 Z = -4740789
25
XDOT = 18802
950205 XDOT = 5731
139222
YDOT = 12183
016263 feet/sec YDOT = 3713
383357 meter/sec
ZDOT = 8953
438874 ZDOT = 2729
008169
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 16101
51126222
00016717 00000-0 10270-3 0 9041
2 25544 51
6421 35
5851 0002639 43
4169 316
7191 15
54432777 34454
Satellite: ISS
Catalog Number: 25544
Epoch time: 16101
51126222 = yrday
fracday
Element set: 904
Inclination: 51
6421 deg
RA of node: 35
5851 deg
Eccentricity:
0002639
Arg of perigee: 43
4169 deg
Mean anomaly: 316
7191 deg
Mean motion: 15
54432777 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3445
Checksum: 289
Coasting Arc #6 (Orbit 3460)
---------------------------------------
Vector Time (GMT): 2016/102/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 944180
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5698582
24 A = 6782781
39 meter
Y = 37046
33 meter E =
0013955
Z = 3669117
58 I = 51
83224
XDOT = -2860
352924 Wp = 78
66339
YDOT = -5619
992773 meter/sec RA = 30
03025 deg
ZDOT = -4369
003383 TA = 57
82040
MA = 57
68512
Ha = 221
334 n
mi
Hp = 213
497
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18696135
94 X = -5716396
15
Y = 121543
07 feet Y = -26778
42 meter
Z = 12037787
34 Z = 3641391
73
XDOT = -9384
359986 XDOT = -2776
073209
YDOT = -18438
296498 feet/sec YDOT = -5651
508130 meter/sec
ZDOT = -14334
000601 ZDOT = -4382
693415
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17679261
43 X = -5388638
88
Y = 6315891
04 feet Y = 1925083
59 meter
Z = 11917291
29 Z = 3632390
38
XDOT = -14400
011175 XDOT = -4389
123406
YDOT = -13046
882977 feet/sec YDOT = -3976
689931 meter/sec
ZDOT = -14392
389594 ZDOT = -4386
800348
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 16102
53988787
00016717 00000-0 10270-3 0 9057
2 25544 51
6427 30
4558 0002565 45
2777 314
8585 15
54454982 34617
Satellite: ISS
Catalog Number: 25544
Epoch time: 16102
53988787 = yrday
fracday
Element set: 905
Inclination: 51
6427 deg
RA of node: 30
4558 deg
Eccentricity:
0002565
Arg of perigee: 45
2777 deg
Mean anomaly: 314
8585 deg
Mean motion: 15
54454982 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3461
Checksum: 338
Coasting Arc #7 (Orbit 3475)
---------------------------------------
Vector Time (GMT): 2016/103/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 944180
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6336854
48 A = 6786427
20 meter
Y = 1081269
61 meter E =
0008953
Z = -2167646
28 I = 51
81644
XDOT = 982
924652 Wp = 43
20091
YDOT = 5241
510019 meter/sec RA = 25
06151 deg
ZDOT = 5507
838398 TA = 292
81415
MA = 292
90869
Ha = 221
317 n
mi
Hp = 213
445
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20790204
99 X = 6334822
05
Y = 3547472
49 feet Y = 1152121
07 meter
Z = -7111700
40 Z = -2136868
19
XDOT = 3224
818412 XDOT = 897
484821
YDOT = 17196
555182 feet/sec YDOT = 5252
024270 meter/sec
ZDOT = 18070
335951 ZDOT = 5512
405467
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20773924
11 X = 6331892
07
Y = -3891371
83 feet Y = -1186090
13 meter
Z = -6978163
75 Z = -2126944
31
XDOT = 8590
631541 XDOT = 2618
424494
YDOT = 13541
232916 feet/sec YDOT = 4127
367793 meter/sec
ZDOT = 18089
146843 ZDOT = 5513
571958
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 16103
50421249
00016717 00000-0 10270-3 0 9061
2 25544 51
6428 25
6463 0002610 48
5111 311
6265 15
54465055 34767
Satellite: ISS
Catalog Number: 25544
Epoch time: 16103
50421249 = yrday
fracday
Element set: 906
Inclination: 51
6428 deg
RA of node: 25
6463 deg
Eccentricity:
0002610
Arg of perigee: 48
5111 deg
Mean anomaly: 311
6265 deg
Mean motion: 15
54465055 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3476
Checksum: 282
Coasting Arc #8 (Orbit 3491)
---------------------------------------
Vector Time (GMT): 2016/104/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 944180
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6453759
62 A = 6788274
90 meter
Y = -2056003
63 meter E =
0013475
Z = 364756
31 I = 51
79382
XDOT = 1125
167869 Wp = 120
03653
YDOT = -4626
610670 meter/sec RA = 20
09985 deg
ZDOT = -6011
329047 TA = 56
03949
MA = 55
91149
Ha = 221
275 n
mi
Hp = 213
364
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21173752
02 X = -6432061
05
Y = -6745418
73 feet Y = -2128052
52 meter
Z = 1196707
04 Z = 333458
23
XDOT = 3691
495632 XDOT = 1206
020733
YDOT = -15179
168866 feet/sec YDOT = -4613
576524 meter/sec
ZDOT = -19722
208158 ZDOT = -6005
666623
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -22185480
16 X = -6762134
35
Y = 1392506
90 feet Y = 424436
10 meter
Z = 1061108
33 Z = 323425
82
XDOT = -1843
633468 XDOT = -561
939481
YDOT = -13914
650308 feet/sec YDOT = -4241
185414 meter/sec
ZDOT = -19696
684094 ZDOT = -6003
549312
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 16104
53281347
00016717 00000-0 10270-3 0 9079
2 25544 51
6433 20
5163 0002608 53
5499 306
5894 15
54475994 34928
Satellite: ISS
Catalog Number: 25544
Epoch time: 16104
53281347 = yrday
fracday
Element set: 907
Inclination: 51
6433 deg
RA of node: 20
5163 deg
Eccentricity:
0002608
Arg of perigee: 53
5499 deg
Mean anomaly: 306
5894 deg
Mean motion: 15
54475994 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3492
Checksum: 321
Coasting Arc #9 (Orbit 3491)
---------------------------------------
Vector Time (GMT): 2016/104/12:24:44
014
Vector Time (MET): N/A
Weight (LBS) : 943981
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1672281
38 A = 6777286
28 meter
Y = -3859803
29 meter E =
0015545
Z = -5327209
73 I = 51
75388
XDOT = 7129
721546 Wp = 86
23664
YDOT = 2783
900258 meter/sec RA = 20
01525 deg
ZDOT = 222
607560 TA = 185
87563
MA = 185
89389
Ha = 221
262 n
mi
Hp = 214
396
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5486487
48 X = 1741195
78
Y = -12663396
61 feet Y = -3840717
67 meter
Z = -17477722
20 Z = -5318918
59
XDOT = 23391
474887 XDOT = 7096
980046
YDOT = 9133
531030 feet/sec YDOT = 2863
446488 meter/sec
ZDOT = 730
339764 ZDOT = 257
162444
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -871360
72 X = -265590
75
Y = -13819866
87 feet Y = -4212295
42 meter
Z = -17440927
22 Z = -5315994
62
XDOT = 23955
607231 XDOT = 7301
669084
YDOT = -2614
489071 feet/sec YDOT = -796
896269 meter/sec
ZDOT = 879
946511 ZDOT = 268
207696
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 16104
53281389
00016717 00000-0 10270-3 0 9086
2 25544 51
6436 20
5161 0001595 25
5858 334
5373 15
54160887 34926
Satellite: ISS
Catalog Number: 25544
Epoch time: 16104
53281389 = yrday
fracday
Element set: 908
Inclination: 51
6436 deg
RA of node: 20
5161 deg
Eccentricity:
0001595
Arg of perigee: 25
5858 deg
Mean anomaly: 334
5373 deg
Mean motion: 15
54160887 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3492
Checksum: 316
Coasting Arc #10 (Orbit 3507)
---------------------------------------
Vector Time (GMT): 2016/105/12:24:44
014
Vector Time (MET): N/A
Weight (LBS) : 943981
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3347198
64 A = 6778720
09 meter
Y = 3162384
67 meter E =
0007660
Z = 4971105
12 I = 51
72828
XDOT = -6487
143803 Wp = 50
40189
YDOT = -3489
965681 meter/sec RA = 15
02402 deg
ZDOT = -2140
875145 TA = 60
45923
MA = 60
38288
Ha = 221
264 n
mi
Hp = 214
335
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10981622
84 X = -3406459
99
Y = 10375277
78 feet Y = 3124623
02 meter
Z = 16309400
01 Z = 4954701
11
XDOT = -21283
280194 XDOT = -6437
236527
YDOT = -11450
018638 feet/sec YDOT = -3562
230319 meter/sec
ZDOT = -7023
868586 ZDOT = -2172
266700
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4806026
39 X = -1464876
84
Y = 14404339
08 feet Y = 4390442
55 meter
Z = 16237490
08 Z = 4949186
98
XDOT = -23077
484683 XDOT = -7034
017331
YDOT = 396
783401 feet/sec YDOT = 120
939581 meter/sec
ZDOT = -7159
582724 ZDOT = -2182
240814
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 16105
56162645
00016717 00000-0 10270-3 0 9094
2 25544 51
6433 15
3882 0001534 22
2445 337
8774 15
54199409 35085
Satellite: ISS
Catalog Number: 25544
Epoch time: 16105
56162645 = yrday
fracday
Element set: 909
Inclination: 51
6433 deg
RA of node: 15
3882 deg
Eccentricity:
0001534
Arg of perigee: 22
2445 deg
Mean anomaly: 337
8774 deg
Mean motion: 15
54199409 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3508
Checksum: 313
Coasting Arc #11 (Orbit 3522)
---------------------------------------
Vector Time (GMT): 2016/106/12:24:44
014
Vector Time (MET): N/A
Weight (LBS) : 943981
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4814059
31 A = 6782090
61 meter
Y = -2444484
83 meter E =
0007645
Z = -4111594
39 I = 51
70946
XDOT = 5295
170663 Wp = 96
68575
YDOT = 4003
668850 meter/sec RA = 10
03637 deg
ZDOT = 3824
768860 TA = 212
78877
MA = 212
83624
Ha = 221
231 n
mi
Hp = 214
406
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15794157
85 X = 4861008
74
Y = -8019963
36 feet Y = -2390388
61 meter
Z = -13489482
91 Z = -4088094
65
XDOT = 17372
607162 XDOT = 5231
427986
YDOT = 13135
396490 feet/sec YDOT = 4062
526846 meter/sec
ZDOT = 12548
454265 ZDOT = 3850
336388
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9890615
69 X = 3014659
66
Y = -14788791
86 feet Y = -4507623
76 meter
Z = -13386886
88 Z = -4080323
12
XDOT = 20436
411925 XDOT = 6229
018355
YDOT = 2224
607757 feet/sec YDOT = 678
060444 meter/sec
ZDOT = 12658
752936 ZDOT = 3858
387895
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 16106
52612755
00016717 00000-0 10270-3 0 9105
2 25544 51
6446 10
5796 0001536 25
6270 334
4958 15
54192349 35235
Satellite: ISS
Catalog Number: 25544
Epoch time: 16106
52612755 = yrday
fracday
Element set: 910
Inclination: 51
6446 deg
RA of node: 10
5796 deg
Eccentricity:
0001536
Arg of perigee: 25
6270 deg
Mean anomaly: 334
4958 deg
Mean motion: 15
54192349 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3523
Checksum: 304
Coasting Arc #12 (Orbit 3538)
---------------------------------------
Vector Time (GMT): 2016/107/12:24:44
014
Vector Time (MET): N/A
Weight (LBS) : 943981
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5950247
20 A = 6785962
41 meter
Y = 1680323
13 meter E =
0014180
Z = 2782647
67 I = 51
69015
XDOT = -3646
671234 Wp = 94
67085
YDOT = -4388
591873 meter/sec RA = 5
05801 deg
ZDOT = -5126
371606 TA = 53
79361
MA = 53
66258
Ha = 221
341 n
mi
Hp = 214
270
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19521808
41 X = -5982111
69
Y = 5512871
15 feet Y = 1613605
58 meter
Z = 9129421
48 Z = 2753665
26
XDOT = -11964
144469 XDOT = -3572
424118
YDOT = -14398
267301 feet/sec YDOT = -4428
956678 meter/sec
ZDOT = -16818
804481 ZDOT = -5143
905542
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14094602
17 X = -4296034
74
Y = 14667117
94 feet Y = 4470537
55 meter
Z = 9003162
19 Z = 2744163
84
XDOT = -16444
446333 XDOT = -5012
267242
YDOT = -5388
753472 feet/sec YDOT = -1642
492058 meter/sec
ZDOT = -16894
115011 ZDOT = -5149
326255
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 16107
55491730
00016717 00000-0 10270-3 0 9118
2 25544 51
6441 5
4514 0001571 34
9341 325
1914 15
54188904 35390
Satellite: ISS
Catalog Number: 25544
Epoch time: 16107
55491730 = yrday
fracday
Element set: 911
Inclination: 51
6441 deg
RA of node: 5
4514 deg
Eccentricity:
0001571
Arg of perigee: 34
9341 deg
Mean anomaly: 325
1914 deg
Mean motion: 15
54188904 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3539
Checksum: 292
Coasting Arc #13 (Orbit 3553)
---------------------------------------
Vector Time (GMT): 2016/108/12:24:44
014
Vector Time (MET): N/A
Weight (LBS) : 943981
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6614485
07 A = 6788462
22 meter
Y = -927704
92 meter E =
0010814
Z = -1185860
98 I = 51
66725
XDOT = 1695
765481 Wp = 36
52116
YDOT = 4639
798960 meter/sec RA =
08605 deg
ZDOT = 5864
878460 TA = 310
60217
MA = 310
69621
Ha = 221
193 n
mi
Hp = 214
227
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21701066
49 X = 6630127
72
Y = -3043651
31 feet Y = -853650
00 meter
Z = -3890620
02 Z = -1153691
26
XDOT = 5563
535042 XDOT = 1615
266885
YDOT = 15222
437532 feet/sec YDOT = 4658
312604 meter/sec
ZDOT = 19241
727231 ZDOT = 5872
920132
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16958245
57 X = 5168873
25
Y = -13917161
74 feet Y = -4241950
90 meter
Z = -3750672
00 Z = -1143204
83
XDOT = 11559
917726 XDOT = 3523
462923
YDOT = 8924
113497 feet/sec YDOT = 2720
069794 meter/sec
ZDOT = 19275
743134 ZDOT = 5875
246507
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 16108
51939565
00016717 00000-0 10270-3 0 9129
2 25544 51
6443
6433 0001484 29
8918 330
2319 15
54234969 35541
Satellite: ISS
Catalog Number: 25544
Epoch time: 16108
51939565 = yrday
fracday
Element set: 912
Inclination: 51
6443 deg
RA of node:
6433 deg
Eccentricity:
0001484
Arg of perigee: 29
8918 deg
Mean anomaly: 330
2319 deg
Mean motion: 15
54234969 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3554
Checksum: 314
Coasting Arc #14 (Orbit 3564)
---------------------------------------
Vector Time (GMT): 2016/109/04:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 943981
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5477566
67 A = 6784382
31 meter
Y = -2292346
80 meter E =
0005794
Z = -3287521
70 I = 51
62837
XDOT = 4508
633089 Wp = 81
87375
YDOT = -4006
468123 meter/sec RA = 356
70910 deg
ZDOT = -4724
822630 TA = 136
28316
MA = 136
23725
Ha = 221
255 n
mi
Hp = 214
050
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17971019
25 X = -5435556
50
Y = -7520822
84 feet Y = -2353366
03 meter
Z = -10785832
34 Z = -3314028
24
XDOT = 14792
103310 XDOT = 4576
050619
YDOT = -13144
580457 feet/sec YDOT = -3955
673103 meter/sec
ZDOT = -15501
386581 ZDOT = -4702
756540
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4829347
04 X = 1471984
98
Y = -18807188
15 feet Y = -5732430
95 meter
Z = -10900530
69 Z = -3322481
75
XDOT = 13806
649508 XDOT = 4208
266770
YDOT = 12461
861468 feet/sec YDOT = 3798
375376 meter/sec
ZDOT = -15404
728481 ZDOT = -4695
361241
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 16109
22667389
00016717 00000-0 10270-3 0 9131
2 25544 51
6409 357
1157 0001536 43
3114 316
8159 15
54220704 35659
Satellite: ISS
Catalog Number: 25544
Epoch time: 16109
22667389 = yrday
fracday
Element set: 913
Inclination: 51
6409 deg
RA of node: 357
1157 deg
Eccentricity:
0001536
Arg of perigee: 43
3114 deg
Mean anomaly: 316
8159 deg
Mean motion: 15
54220704 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3565
Checksum: 304
Coasting Arc #15 (Orbit 3580)
---------------------------------------
Vector Time (GMT): 2016/110/04:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 943981
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4159381
69 A = 6780444
25 meter
Y = 2963465
49 meter E =
0009597
Z = 4453075
93 I = 51
58353
XDOT = -5997
808580 Wp = 102
43773
YDOT = 3493
127439 meter/sec RA = 351
72034 deg
ZDOT = 3269
626455 TA = 314
57367
MA = 314
65197
Ha = 221
094 n
mi
Hp = 214
102
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13646265
40 X = 4104303
02
Y = 9722655
82 feet Y = 3009670
95 meter
Z = 14609829
17 Z = 4473147
28
XDOT = -19677
849672 XDOT = -6052
306420
YDOT = 11460
391859 feet/sec YDOT = 3425
751562 meter/sec
ZDOT = 10727
120914 ZDOT = 3240
357612
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7386398
89 X = -2251374
38
Y = 14955057
23 feet Y = 4558301
44 meter
Z = 14696430
82 Z = 4479472
11
XDOT = -13434
498391 XDOT = -4094
835110
YDOT = -17076
933843 feet/sec YDOT = -5205
049435 meter/sec
ZDOT = 10599
284367 ZDOT = 3230
661875
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 16110
25543234
00016717 00000-0 10270-3 0 9149
2 25544 51
6408 351
9872 0001511 39
2947 320
8315 15
54253076 35810
Satellite: ISS
Catalog Number: 25544
Epoch time: 16110
25543234 = yrday
fracday
Element set: 914
Inclination: 51
6408 deg
RA of node: 351
9872 deg
Eccentricity:
0001511
Arg of perigee: 39
2947 deg
Mean anomaly: 320
8315 deg
Mean motion: 15
54253076 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3581
Checksum: 293
Coasting Arc #16 (Orbit 3595)
---------------------------------------
Vector Time (GMT): 2016/111/04:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 943981
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2527402
31 A = 6777651
46 meter
Y = -3614328
83 meter E =
0015218
Z = -5159973
95 I = 51
54181
XDOT = 6971
880782 Wp = 75
45759
YDOT = -2820
228095 meter/sec RA = 346
71872 deg
ZDOT = -1439
273441 TA = 180
65268
MA = 180
65467
Ha = 221
260 n
mi
Hp = 213
961
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8292002
32 X = -2461732
88
Y = -11858034
23 feet Y = -3642225
24 meter
Z = -16929048
39 Z = -5172091
75
XDOT = 22873
624612 XDOT = 7009
890570
YDOT = -9252
716848 feet/sec YDOT = -2742
051495 meter/sec
ZDOT = -4722
025724 ZDOT = -1405
312768
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10194461
69 X = 3107271
92
Y = -10182469
12 feet Y = -3103616
59 meter
Z = -16980966
73 Z = -5175798
66
XDOT = 12478
981106 XDOT = 3803
593441
YDOT = 20122
463578 feet/sec YDOT = 6133
326899 meter/sec
ZDOT = -4573
953723 ZDOT = -1394
141095
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 16111
21988626
00016717 00000-0 10270-3 0 9155
2 25544 51
6402 347
1787 0001612 44
7782 315
3501 15
54249004 35964
Satellite: ISS
Catalog Number: 25544
Epoch time: 16111
21988626 = yrday
fracday
Element set: 915
Inclination: 51
6402 deg
RA of node: 347
1787 deg
Eccentricity:
0001612
Arg of perigee: 44
7782 deg
Mean anomaly: 315
3501 deg
Mean motion: 15
54249004 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3596
Checksum: 303
Coasting Arc #17 (Orbit 3611)
---------------------------------------
Vector Time (GMT): 2016/112/04:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 943981
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 733916
41 A = 6777065
64 meter
Y = 4180001
96 meter E =
0004334
Z = 5280700
56 I = 51
50868
XDOT = -7389
975740 Wp = 58
15219
YDOT = 1987
380869 meter/sec RA = 341
71006 deg
ZDOT = -543
500391 TA = 37
05581
MA = 37
02589
Ha = 221
189 n
mi
Hp = 214
054
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2407862
24 X = 661468
26
Y = 13713917
19 feet Y = 4187804
46 meter
Z = 17325133
06 Z = 5284089
48
XDOT = -24245
327231 XDOT = -7409
009754
YDOT = 6520
278442 feet/sec YDOT = 1904
634772 meter/sec
ZDOT = -1783
137767 ZDOT = -579
446014
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12995606
03 X = -3961060
72
Y = 4949955
82 feet Y = 1508746
53 meter
Z = 17339023
10 Z = 5284934
24
XDOT = -10799
537277 XDOT = -3291
698962
YDOT = -21529
236332 feet/sec YDOT = -6562
111234 meter/sec
ZDOT = -1939
654337 ZDOT = -591
206642
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 16112
24862834
00016717 00000-0 10270-3 0 9162
2 25544 51
6399 342
0497 0001520 44
6353 315
4922 15
54264244 36122
Satellite: ISS
Catalog Number: 25544
Epoch time: 16112
24862834 = yrday
fracday
Element set: 916
Inclination: 51
6399 deg
RA of node: 342
0497 deg
Eccentricity:
0001520
Arg of perigee: 44
6353 deg
Mean anomaly: 315
4922 deg
Mean motion: 15
54264244 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3612
Checksum: 298
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