[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
August 28th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 11840 3 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 122 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 819 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
243/07:13:07
286 0
7 1
7 1
7
N/A 1
5 0
1 219
2
000/00:08:14
572 -0
2 -0
1 213
1
245/10:53:00
000 0
0 0
0 0
0
N/A 0
0 0
0 219
3
000/00:00:00
000 0
0 0
0 213
0
250/04:11:17
943 0
8 0
9 0
9
N/A 0
4 0
0 219
0
000/00:04:31
886 -0
2 0
0 213
3
Coasting Arc #1 (Orbit 3898)
---------------------------------------
Vector Time (GMT): 2015/238/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 927198
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -628934
16 A = 6785300
44 meter
Y = 6731869
78 meter E =
0014014
Z = 487381
60 I = 52
02795
XDOT = -4670
986719 Wp = 51
57869
YDOT = -880
214138 meter/sec RA = 92
11213 deg
ZDOT = 6022
103358 TA = 313
65430
MA = 313
77041
Ha = 219
267 n
mi
Hp = 212
173
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2063432
28 X = -706532
29
Y = 22086186
94 feet Y = 6724402
76 meter
Z = 1599021
00 Z = 484137
74
XDOT = -15324
759577 XDOT = -4690
049493
YDOT = -2887
841661 feet/sec YDOT = -932
554599 meter/sec
ZDOT = 19757
556949 ZDOT = 5999
366666
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11684366
15 X = 3561394
80
Y = -18856865
34 feet Y = -5747572
56 meter
Z = 1583821
86 Z = 482748
90
XDOT = 11177
557654 XDOT = 3406
919573
YDOT = 8607
320905 feet/sec YDOT = 2623
511412 meter/sec
ZDOT = 19659
632835 ZDOT = 5992
256088
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 15238
56331913
00016717 00000-0 10270-3 0 9007
2 25544 51
6430 92
6469 0001117 67
5674 292
5598 15
55482499 38993
Satellite: ISS
Catalog Number: 25544
Epoch time: 15238
56331913 = yrday
fracday
Element set: 900
Inclination: 51
6430 deg
RA of node: 92
6469 deg
Eccentricity:
0001117
Arg of perigee: 67
5674 deg
Mean anomaly: 292
5598 deg
Mean motion: 15
55482499 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3899
Checksum: 344
Coasting Arc #2 (Orbit 3913)
---------------------------------------
Vector Time (GMT): 2015/239/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 927198
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1715363
94 A = 6782623
35 meter
Y = -6034698
13 meter E =
0005756
Z = -2577444
84 I = 52
01826
XDOT = 4312
522365 Wp = 119
55101
YDOT = 3482
609378 meter/sec RA = 87
15866 deg
ZDOT = -5295
507188 TA = 89
27292
MA = 89
20696
Ha = 219
261 n
mi
Hp = 212
230
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5627834
45 X = 1795237
95
Y = -19798878
39 feet Y = -6015069
32 meter
Z = -8456183
86 Z = -2568917
80
XDOT = 14148
695422 XDOT = 4298
981619
YDOT = 11425
883786 feet/sec YDOT = 3530
758883 meter/sec
ZDOT = -17373
711248 ZDOT = -5274
591203
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13634558
73 X = -4155813
50
Y = 15440401
58 feet Y = 4706234
40 meter
Z = -8418310
93 Z = -2565901
17
XDOT = -6844
739427 XDOT = -2086
276577
YDOT = -15446
868668 feet/sec YDOT = -4708
205570 meter/sec
ZDOT = -17284
106457 ZDOT = -5268
195648
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 15239
52701398
00016717 00000-0 10270-3 0 9013
2 25544 51
6421 87
8329 0001050 68
5189 291
6076 15
55473490 39142
Satellite: ISS
Catalog Number: 25544
Epoch time: 15239
52701398 = yrday
fracday
Element set: 901
Inclination: 51
6421 deg
RA of node: 87
8329 deg
Eccentricity:
0001050
Arg of perigee: 68
5189 deg
Mean anomaly: 291
6076 deg
Mean motion: 15
55473490 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3914
Checksum: 319
Coasting Arc #3 (Orbit 3929)
---------------------------------------
Vector Time (GMT): 2015/240/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 927198
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2696170
26 A = 6777903
10 meter
Y = 4566617
54 meter E =
0011076
Z = 4213126
42 I = 51
99950
XDOT = -3694
224209 Wp = 101
57315
YDOT = -5611
986288 meter/sec RA = 82
18996 deg
ZDOT = 3708
369528 TA = 310
55565
MA = 310
65203
Ha = 219
327 n
mi
Hp = 212
175
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8845702
97 X = -2767500
32
Y = 14982341
01 feet Y = 4536068
66 meter
Z = 13822593
25 Z = 4199855
62
XDOT = -12120
158166 XDOT = -3649
208603
YDOT = -18412
028503 feet/sec YDOT = -5653
045576 meter/sec
ZDOT = 12166
566694 ZDOT = 3690
533763
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14334097
18 X = 4369032
82
Y = -9942478
96 feet Y = -3030467
59 meter
Z = 13764514
42 Z = 4195424
00
XDOT = 2758
793268 XDOT = 840
880188
YDOT = 20763
133041 feet/sec YDOT = 6328
602951 meter/sec
ZDOT = 12090
636078 ZDOT = 3685
225877
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 15240
55494214
00016717 00000-0 10270-3 0 9025
2 25544 51
6415 82
6966 0001110 65
9527 294
1743 15
55485198 39304
Satellite: ISS
Catalog Number: 25544
Epoch time: 15240
55494214 = yrday
fracday
Element set: 902
Inclination: 51
6415 deg
RA of node: 82
6966 deg
Eccentricity:
0001110
Arg of perigee: 65
9527 deg
Mean anomaly: 294
1743 deg
Mean motion: 15
55485198 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3930
Checksum: 313
Coasting Arc #4 (Orbit 3944)
---------------------------------------
Vector Time (GMT): 2015/241/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 927198
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3579987
18 A = 6774010
13 meter
Y = -2524336
02 meter E =
0014852
Z = -5180240
59 I = 51
98018
XDOT = 2776
153535 Wp = 78
43376
YDOT = 6982
602528 meter/sec RA = 77
20521 deg
ZDOT = -1484
766423 TA = 177
32571
MA = 177
31776
Ha = 219
193 n
mi
Hp = 212
203
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11745364
77 X = 3633112
09
Y = -8281942
31 feet Y = -2484005
69 meter
Z = -16995539
99 Z = -5162720
73
XDOT = 9108
115272 XDOT = 2705
078373
YDOT = 22908
800944 feet/sec YDOT = 7013
249760 meter/sec
ZDOT = -4871
280916 ZDOT = -1471
453922
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14171634
25 X = -4319514
12
Y = 2878879
08 feet Y = 877482
34 meter
Z = -16919497
03 Z = -5157062
69
XDOT = 947
852389 XDOT = 288
905408
YDOT = -23619
588209 feet/sec YDOT = -7199
250486 meter/sec
ZDOT = -4815
117940 ZDOT = -1467
647948
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 15241
51861113
00016717 00000-0 10270-3 0 9039
2 25544 51
6402 77
8813 0001088 74
7015 285
4259 15
55524148 39451
Satellite: ISS
Catalog Number: 25544
Epoch time: 15241
51861113 = yrday
fracday
Element set: 903
Inclination: 51
6402 deg
RA of node: 77
8813 deg
Eccentricity:
0001088
Arg of perigee: 74
7015 deg
Mean anomaly: 285
4259 deg
Mean motion: 15
55524148 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3945
Checksum: 304
Coasting Arc #5 (Orbit 3960)
---------------------------------------
Vector Time (GMT): 2015/242/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 927198
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4255925
29 A = 6773612
23 meter
Y = 206873
75 meter E =
0004594
Z = 5262360
60 I = 51
97115
XDOT = -1580
891046 Wp = 62
42083
YDOT = -7444
697638 meter/sec RA = 72
21269 deg
ZDOT = -983
151235 TA = 36
95545
MA = 36
92381
Ha = 219
338 n
mi
Hp = 212
098
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13963009
47 X = -4283484
53
Y = 678719
65 feet Y = 159127
68 meter
Z = 17264962
59 Z = 5241619
46
XDOT = -5186
650413 XDOT = -1492
749423
YDOT = -24424
861018 feet/sec YDOT = -7461
883482 meter/sec
ZDOT = -3225
561794 ZDOT = -990
615888
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13263832
55 X = 4042816
16
Y = 4751848
85 feet Y = 1448363
53 meter
Z = 17175444
84 Z = 5235075
59
XDOT = -4218
355667 XDOT = -1285
754807
YDOT = 23577
383407 feet/sec YDOT = 7186
386462 meter/sec
ZDOT = -3256
403984 ZDOT = -992
551934
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 15242
54651277
00016717 00000-0 10270-3 0 9042
2 25544 51
6404 72
7454 0001054 78
8574 281
2698 15
55523590 39615
Satellite: ISS
Catalog Number: 25544
Epoch time: 15242
54651277 = yrday
fracday
Element set: 904
Inclination: 51
6404 deg
RA of node: 72
7454 deg
Eccentricity:
0001054
Arg of perigee: 78
8574 deg
Mean anomaly: 281
2698 deg
Mean motion: 15
55523590 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3961
Checksum: 321
Coasting Arc #6 (Orbit 3972)
---------------------------------------
Vector Time (GMT): 2015/243/07:17:14
572
Vector Time (MET): N/A
Weight (LBS) : 927020
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4338764
20 A = 6774662
97 meter
Y = -132229
13 meter E =
0013750
Z = -5213423
07 I = 51
96706
XDOT = 1812
298869 Wp = 99
29040
YDOT = 7323
942043 meter/sec RA = 68
21597 deg
ZDOT = 1323
297648 TA = 183
37445
MA = 183
38373
Ha = 219
165 n
mi
Hp = 213
096
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14234790
68 X = 4365244
97
Y = -433822
61 feet Y = -83562
76 meter
Z = -17104406
41 Z = -5192282
07
XDOT = 5945
862431 XDOT = 1723
838059
YDOT = 24028
681242 feet/sec YDOT = 7343
713901 meter/sec
ZDOT = 4341
527715 ZDOT = 1331
885649
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 159424
59 X = 48592
61
Y = -14349372
95 feet Y = -4373688
88 meter
Z = -17013179
19 Z = -5185617
02
XDOT = 23207
301969 XDOT = 7073
585640
YDOT = -4928
818114 feet/sec YDOT = -1502
303761 meter/sec
ZDOT = 4377
229888 ZDOT = 1334
179670
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 15243
31743126
00016717 00000-0 10270-3 0 9054
2 25544 51
6438 68
8960 0000276 319
4255 40
6877 15
55256212 39738
Satellite: ISS
Catalog Number: 25544
Epoch time: 15243
31743126 = yrday
fracday
Element set: 905
Inclination: 51
6438 deg
RA of node: 68
8960 deg
Eccentricity:
0000276
Arg of perigee: 319
4255 deg
Mean anomaly: 40
6877 deg
Mean motion: 15
55256212 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3973
Checksum: 316
Coasting Arc #7 (Orbit 3988)
---------------------------------------
Vector Time (GMT): 2015/244/07:17:14
572
Vector Time (MET): N/A
Weight (LBS) : 927020
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4804838
22 A = 6778019
22 meter
Y = -1967476
58 meter E =
0009641
Z = 4351369
98 I = 51
96594
XDOT = -379
668387 Wp = 69
44733
YDOT = -6820
672336 meter/sec RA = 63
23200 deg
ZDOT = -3493
676194 TA = 55
91511
MA = 55
82365
Ha = 219
228 n
mi
Hp = 212
932
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15763904
93 X = -4803617
54
Y = -6454975
66 feet Y = -2021200
13 meter
Z = 14276148
22 Z = 4328032
32
XDOT = -1245
631190 XDOT = -286
398875
YDOT = -22377
533912 feet/sec YDOT = -6824
396931 meter/sec
ZDOT = -11462
192238 ZDOT = -3495
293231
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6836238
27 X = -2083685
42
Y = 15693543
36 feet Y = 4783392
02 meter
Z = 14175837
21 Z = 4320795
18
XDOT = -21256
019530 XDOT = -6478
834753
YDOT = 1128
005627 feet/sec YDOT = 343
816115 meter/sec
ZDOT = -11467
903008 ZDOT = -3495
416837
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 15244
34551613
00016717 00000-0 10270-3 0 9067
2 25544 51
6438 63
7618 0000405 330
3692 29
7439 15
55289887 39896
Satellite: ISS
Catalog Number: 25544
Epoch time: 15244
34551613 = yrday
fracday
Element set: 906
Inclination: 51
6438 deg
RA of node: 63
7618 deg
Eccentricity:
0000405
Arg of perigee: 330
3692 deg
Mean anomaly: 29
7439 deg
Mean motion: 15
55289887 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3989
Checksum: 337
Coasting Arc #8 (Orbit 4003)
---------------------------------------
Vector Time (GMT): 2015/245/07:17:14
572
Vector Time (MET): N/A
Weight (LBS) : 927020
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4910857
59 A = 6782596
58 meter
Y = 3718530
19 meter E =
0004701
Z = -2838468
15 I = 51
96685
XDOT = -1262
836762 Wp = 54
31810
YDOT = 5567
157409 meter/sec RA = 58
26081 deg
ZDOT = 5116
994441 TA = 273
58646
MA = 273
64023
Ha = 219
114 n
mi
Hp = 212
999
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16111737
50 X = 4882699
29
Y = 12199902
20 feet Y = 3773288
90 meter
Z = -9312559
56 Z = -2814680
98
XDOT = -4143
165231 XDOT = -1349
852604
YDOT = 18264
952128 feet/sec YDOT = 5552
549517 meter/sec
ZDOT = 16788
039504 ZDOT = 5110
647926
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12312733
07 X = 3752921
04
Y = -16084467
65 feet Y = -4902545
74 meter
Z = -9210644
34 Z = -2807404
39
XDOT = 17063
151176 XDOT = 5200
848479
YDOT = 3480
979879 feet/sec YDOT = 1061
002667 meter/sec
ZDOT = 16759
619677 ZDOT = 5108
332077
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 15245
30933348
00016717 00000-0 10270-3 0 9074
2 25544 51
6446 58
9482 0000482 326
5242 33
5881 15
55293081 40047
Satellite: ISS
Catalog Number: 25544
Epoch time: 15245
30933348 = yrday
fracday
Element set: 907
Inclination: 51
6446 deg
RA of node: 58
9482 deg
Eccentricity:
0000482
Arg of perigee: 326
5242 deg
Mean anomaly: 33
5881 deg
Mean motion: 15
55293081 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4004
Checksum: 305
Coasting Arc #9 (Orbit 4006)
---------------------------------------
Vector Time (GMT): 2015/245/10:53:00
000
Vector Time (MET): N/A
Weight (LBS) : 941307
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3358014
12 A = 6774089
38 meter
Y = 2493775
35 meter E =
0002184
Z = 5326657
53 I = 51
93205
XDOT = -4291
746935 Wp = 95
81815
YDOT = -6354
208698 meter/sec RA = 57
53832 deg
ZDOT = 268
943497 TA = 351
62814
MA = 351
63178
Ha = 219
259 n
mi
Hp = 212
996
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11017106
68 X = -3411525
41
Y = 8181677
65 feet Y = 2455925
15 meter
Z = 17475910
52 Z = 5310214
75
XDOT = -14080
534564 XDOT = -4221
680088
YDOT = -20847
141396 feet/sec YDOT = -6401
810043 meter/sec
ZDOT = 882
360555 ZDOT = 248
265869
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13813284
99 X = 4210289
27
Y = -2884
01 feet Y = -879
05 meter
Z = 17404513
40 Z = 5304895
68
XDOT = -997
123176 XDOT = -303
923144
YDOT = 24132
697141 feet/sec YDOT = 7355
646088 meter/sec
ZDOT = 794
354891 ZDOT = 242
119371
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 15245
50209568
00016717 00000-0 10270-3 0 9087
2 25544 51
6410 57
9830 0000373 313
6609 46
4513 15
55253944 40079
Satellite: ISS
Catalog Number: 25544
Epoch time: 15245
50209568 = yrday
fracday
Element set: 908
Inclination: 51
6410 deg
RA of node: 57
9830 deg
Eccentricity:
0000373
Arg of perigee: 313
6609 deg
Mean anomaly: 46
4513 deg
Mean motion: 15
55253944 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4007
Checksum: 300
Coasting Arc #10 (Orbit 4021)
---------------------------------------
Vector Time (GMT): 2015/246/10:53:00
000
Vector Time (MET): N/A
Weight (LBS) : 941307
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4541014
67 A = 6775366
80 meter
Y = -529848
20 meter E =
0012307
Z = -5011640
54 I = 51
91847
XDOT = 3077
599011 Wp = 104
45836
YDOT = 6699
429392 meter/sec RA = 52
54500 deg
ZDOT = 2081
580626 TA = 185
72875
MA = 185
74284
Ha = 219
059 n
mi
Hp = 213
022
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14898342
10 X = 4570946
73
Y = -1738347
10 feet Y = -478900
64 meter
Z = -16442390
22 Z = -4989508
44
XDOT = 10097
109617 XDOT = 2992
344101
YDOT = 21979
755222 feet/sec YDOT = 6733
368612 meter/sec
ZDOT = 6829
332761 ZDOT = 2096
323367
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13245903
17 X = -4037351
29
Y = -7256868
75 feet Y = -2211893
59 meter
Z = -16346820
77 Z = -4982510
97
XDOT = 3980
389747 XDOT = 1213
222795
YDOT = -22780
038172 feet/sec YDOT = -6943
355635 meter/sec
ZDOT = 6891
657780 ZDOT = 2100
577291
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 15246
46589778
00016717 00000-0 10270-3 0 9098
2 25544 51
6406 53
1685 0000327 314
8345 45
2782 15
55313855 40229
Satellite: ISS
Catalog Number: 25544
Epoch time: 15246
46589778 = yrday
fracday
Element set: 909
Inclination: 51
6406 deg
RA of node: 53
1685 deg
Eccentricity:
0000327
Arg of perigee: 314
8345 deg
Mean anomaly: 45
2782 deg
Mean motion: 15
55313855 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4022
Checksum: 321
Coasting Arc #11 (Orbit 4037)
---------------------------------------
Vector Time (GMT): 2015/247/10:53:00
000
Vector Time (MET): N/A
Weight (LBS) : 941307
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5376777
93 A = 6779526
04 meter
Y = -1361314
67 meter E =
0010997
Z = 3890897
00 I = 51
91267
XDOT = -1394
699880 Wp = 79
49463
YDOT = -6317
068119 meter/sec RA = 47
56154 deg
ZDOT = -4125
654302 TA = 53
64759
MA = 53
54614
Ha = 219
095 n
mi
Hp = 212
944
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17640347
54 X = -5380056
27
Y = -4466255
47 feet Y = -1421459
40 meter
Z = 12765410
10 Z = 3864769
82
XDOT = -4575
787008 XDOT = -1303
916376
YDOT = -20725
289104 feet/sec YDOT = -6332
157255 meter/sec
ZDOT = -13535
611227 ZDOT = -4132
208536
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12112569
13 X = 3691911
07
Y = 13684772
79 feet Y = 4171118
75 meter
Z = 12652970
30 Z = 3856625
35
XDOT = -6989
044227 XDOT = -2130
260680
YDOT = 18762
363713 feet/sec YDOT = 5718
768460 meter/sec
ZDOT = -13562
674868 ZDOT = -4133
903300
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 15247
49394030
00016717 00000-0 10270-3 0 9109
2 25544 51
6409 48
0343 0000481 309
8714 50
2397 15
55327365 40387
Satellite: ISS
Catalog Number: 25544
Epoch time: 15247
49394030 = yrday
fracday
Element set: 910
Inclination: 51
6409 deg
RA of node: 48
0343 deg
Eccentricity:
0000481
Arg of perigee: 309
8714 deg
Mean anomaly: 50
2397 deg
Mean motion: 15
55327365 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4038
Checksum: 300
Coasting Arc #12 (Orbit 4052)
---------------------------------------
Vector Time (GMT): 2015/248/10:53:00
000
Vector Time (MET): N/A
Weight (LBS) : 941307
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5713860
49 A = 6783822
21 meter
Y = 2931887
53 meter E =
0006396
Z = -2179252
39 I = 51
90514
XDOT = -621
261588 Wp = 38
69948
YDOT = 5296
057431 meter/sec RA = 42
59089 deg
ZDOT = 5509
786510 TA = 297
20175
MA = 297
26693
Ha = 219
055 n
mi
Hp = 212
859
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18746261
44 X = 5691236
70
Y = 9619053
57 feet Y = 2995657
05 meter
Z = -7149778
17 Z = -2151550
78
XDOT = -2038
259804 XDOT = -707
201610
YDOT = 17375
516507 feet/sec YDOT = 5288
629892 meter/sec
ZDOT = 18076
727394 ZDOT = 5506
559489
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10406128
24 X = -3171787
89
Y = -18367020
19 feet Y = -5598267
75 meter
Z = -7030853
55 Z = -2143004
16
XDOT = 10015
050562 XDOT = 3052
587411
YDOT = -12570
866574 feet/sec YDOT = -3831
600132 meter/sec
ZDOT = 18061
786775 ZDOT = 5505
232609
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 15248
45771848
00016717 00000-0 10270-3 0 9113
2 25544 51
6409 43
2200 0000322 326
2425 33
8708 15
55351426 40537
Satellite: ISS
Catalog Number: 25544
Epoch time: 15248
45771848 = yrday
fracday
Element set: 911
Inclination: 51
6409 deg
RA of node: 43
2200 deg
Eccentricity:
0000322
Arg of perigee: 326
2425 deg
Mean anomaly: 33
8708 deg
Mean motion: 15
55351426 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4053
Checksum: 284
Coasting Arc #13 (Orbit 4068)
---------------------------------------
Vector Time (GMT): 2015/249/10:53:00
000
Vector Time (MET): N/A
Weight (LBS) : 941307
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5409831
83 A = 6785584
26 meter
Y = -4086204
03 meter E =
0011653
Z = 85383
61 I = 51
88756
XDOT = 2787
818274 Wp = 132
29861
YDOT = -3827
755418 meter/sec RA = 37
63088 deg
ZDOT = -6034
280210 TA = 46
78430
MA = 46
68704
Ha = 218
898 n
mi
Hp = 212
744
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17748792
10 X = -5364151
60
Y = -13406181
19 feet Y = -4146444
91 meter
Z = 280129
95 Z = 59215
05
XDOT = 9146
385414 XDOT = 2859
726070
YDOT = -12558
252684 feet/sec YDOT = -3796
178499 meter/sec
ZDOT = -19797
507251 ZDOT = -6020
562726
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7812938
71 X = 2381383
72
Y = 20826750
51 feet Y = 6347993
56 meter
Z = 168046
97 Z = 51220
72
XDOT = -13037
847450 XDOT = -3973
935903
YDOT = 5073
080853 feet/sec YDOT = 1546
275044 meter/sec
ZDOT = -19737
595842 ZDOT = -6016
019213
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 15249
48573252
00016717 00000-0 10270-3 0 9127
2 25544 51
6408 38
0853 0000628 339
3482 20
7646 15
55417293 40697
Satellite: ISS
Catalog Number: 25544
Epoch time: 15249
48573252 = yrday
fracday
Element set: 912
Inclination: 51
6408 deg
RA of node: 38
0853 deg
Eccentricity:
0000628
Arg of perigee: 339
3482 deg
Mean anomaly: 20
7646 deg
Mean motion: 15
55417293 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4069
Checksum: 318
Coasting Arc #14 (Orbit 4079)
---------------------------------------
Vector Time (GMT): 2015/250/04:13:33
886
Vector Time (MET): N/A
Weight (LBS) : 941209
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2132424
99 A = 6774141
24 meter
Y = -3614736
44 meter E =
0014073
Z = -5329594
03 I = 51
83296
XDOT = 6442
978982 Wp = 85
50685
YDOT = 4136
743252 meter/sec RA = 34
03934 deg
ZDOT = -227
239317 TA = 182
32746
MA = 182
33402
Ha = 218
967 n
mi
Hp = 213
293
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6996144
99 X = 2198576
33
Y = -11859371
52 feet Y = -3590520
72 meter
Z = -17485544
71 Z = -5319074
30
XDOT = 21138
382486 XDOT = 6397
345896
YDOT = 13571
992296 feet/sec YDOT = 4208
537719 meter/sec
ZDOT = -745
535816 ZDOT = -196
051921
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4168851
12 X = -1270665
82
Y = -13184108
07 feet Y = -4018516
14 meter
Z = -17439466
34 Z = -5315549
34
XDOT = 23215
465191 XDOT = 7076
073790
YDOT = -6529
073885 feet/sec YDOT = -1990
061720 meter/sec
ZDOT = -611
818723 ZDOT = -186
482347
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 15250
19248689
00016717 00000-0 10270-3 0 9131
2 25544 51
6446 34
5598 0001043 307
3189 52
7870 15
55236983 40809
Satellite: ISS
Catalog Number: 25544
Epoch time: 15250
19248689 = yrday
fracday
Element set: 913
Inclination: 51
6446 deg
RA of node: 34
5598 deg
Eccentricity:
0001043
Arg of perigee: 307
3189 deg
Mean anomaly: 52
7870 deg
Mean motion: 15
55236983 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4080
Checksum: 324
Coasting Arc #15 (Orbit 4095)
---------------------------------------
Vector Time (GMT): 2015/251/04:13:33
886
Vector Time (MET): N/A
Weight (LBS) : 941209
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3971619
70 A = 6775510
79 meter
Y = 2283947
93 meter E =
0006025
Z = 4989390
87 I = 51
81074
XDOT = -5484
882758 Wp = 45
35576
YDOT = -4935
744045 meter/sec RA = 29
04081 deg
ZDOT = -2100
958254 TA = 65
06616
MA = 65
00357
Ha = 219
000 n
mi
Hp = 213
202
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13030248
36 X = -4021100
52
Y = 7493267
49 feet Y = 2239258
36 meter
Z = 16369392
63 Z = 4969977
37
XDOT = -17995
022173 XDOT = -5419
076862
YDOT = -16193
385973 feet/sec YDOT = -4996
711821 meter/sec
ZDOT = -6892
907658 ZDOT = -2127
442283
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2840282
85 X = -865718
21
Y = 14853218
61 feet Y = 4527261
03 meter
Z = 16285212
17 Z = 4963732
67
XDOT = -22890
859823 XDOT = -6977
134074
YDOT = 3324
941062 feet/sec YDOT = 1013
442036 meter/sec
ZDOT = -7006
176418 ZDOT = -2135
482572
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 15251
22058755
00016717 00000-0 10270-3 0 9140
2 25544 51
6444 29
4260 0001237 311
5324 48
5723 15
55279073 40963
Satellite: ISS
Catalog Number: 25544
Epoch time: 15251
22058755 = yrday
fracday
Element set: 914
Inclination: 51
6444 deg
RA of node: 29
4260 deg
Eccentricity:
0001237
Arg of perigee: 311
5324 deg
Mean anomaly: 48
5723 deg
Mean motion: 15
55279073 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4096
Checksum: 297
Coasting Arc #16 (Orbit 4110)
---------------------------------------
Vector Time (GMT): 2015/252/04:13:33
886
Vector Time (MET): N/A
Weight (LBS) : 941209
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5470581
93 A = 6779673
54 meter
Y = -921658
33 meter E =
0005303
Z = -3902179
15 I = 51
79673
XDOT = 3806
477865 Wp = 97
55378
YDOT = 5235
580210 meter/sec RA = 24
04971 deg
ZDOT = 4103
912813 TA = 215
38117
MA = 215
41637
Ha = 218
960 n
mi
Hp = 213
298
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17948103
46 X = 5499436
66
Y = -3023813
43 feet Y = -860321
68 meter
Z = -12802425
04 Z = -3875534
28
XDOT = 12488
444439 XDOT = 3727
714396
YDOT = 17177
100428 feet/sec YDOT = 5277
706708 meter/sec
ZDOT = 13464
280881 ZDOT = 4122
211972
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9147763
56 X = 2788238
33
Y = -15828145
45 feet Y = -4824418
73 meter
Z = -12687323
82 Z = -3867096
30
XDOT = 19988
614494 XDOT = 6092
529698
YDOT = 708
165754 feet/sec YDOT = 215
848922 meter/sec
ZDOT = 13542
183684 ZDOT = 4127
657587
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 15252
18442014
00016717 00000-0 10270-3 0 9152
2 25544 51
6449 24
6126 0001273 316
7221 43
3832 15
55267674 41115
Satellite: ISS
Catalog Number: 25544
Epoch time: 15252
18442014 = yrday
fracday
Element set: 915
Inclination: 51
6449 deg
RA of node: 24
6126 deg
Eccentricity:
0001273
Arg of perigee: 316
7221 deg
Mean anomaly: 43
3832 deg
Mean motion: 15
55267674 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4111
Checksum: 281
Coasting Arc #17 (Orbit 4126)
---------------------------------------
Vector Time (GMT): 2015/253/04:13:33
886
Vector Time (MET): N/A
Weight (LBS) : 941209
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6404627
67 A = 6784078
93 meter
Y = -394430
28 meter E =
0012950
Z = 2184292
44 I = 51
78198
XDOT = -1566
607724 Wp = 106
46995
YDOT = -5119
548451 meter/sec RA = 19
07209 deg
ZDOT = -5494
603801 TA = 49
31529
MA = 49
20283
Ha = 219
031 n
mi
Hp = 213
177
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21012557
98 X = -6410351
40
Y = -1294062
59 feet Y = -466082
82 meter
Z = 7166313
79 Z = 2153166
52
XDOT = -5139
789122 XDOT = -1482
552847
YDOT = -16796
418801 feet/sec YDOT = -5136
597863 meter/sec
ZDOT = -18026
915358 ZDOT = -5502
009313
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14138621
84 X = -4309451
94
Y = 15659070
64 feet Y = 4772884
73 meter
Z = 7032149
28 Z = 2143399
10
XDOT = -15124
982324 XDOT = -4610
094612
YDOT = -5511
928525 feet/sec YDOT = -1680
035814 meter/sec
ZDOT = -18057
854056 ZDOT = -5504
033916
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 15253
21249423
00016717 00000-0 10270-3 0 9167
2 25544 51
6449 19
4786 0001167 322
9142 37
1931 15
55265137 41272
Satellite: ISS
Catalog Number: 25544
Epoch time: 15253
21249423 = yrday
fracday
Element set: 916
Inclination: 51
6449 deg
RA of node: 19
4786 deg
Eccentricity:
0001167
Arg of perigee: 322
9142 deg
Mean anomaly: 37
1931 deg
Mean motion: 15
55265137 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4127
Checksum: 303
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