[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
May 10th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 16145 87 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 127 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 568 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
136/01:11:19
980 -4
0 5
0 5
0
N/A -1
0 -0
7 218
3
000/00:14:39
961 -2
9 -0
2 216
2
Coasting Arc #1 (Orbit 2186)
---------------------------------------
Vector Time (GMT): 2015/128/12:13:12
993
Vector Time (MET): N/A
Weight (LBS) : 911686
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4365044
47 A = 6773830
49 meter
Y = -1074997
91 meter E =
0002658
Z = 5069474
66 I = 51
27073
XDOT = -125
515123 Wp = 243
65283
YDOT = 7478
622938 meter/sec RA = 281
42322 deg
ZDOT = 1693
470931 TA = 189
90144
MA = 189
90668
Ha = 216
763 n
mi
Hp = 214
920
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14321012
04 X = 4352115
03
Y = -3526896
02 feet Y = -1026257
62 meter
Z = 16632134
71 Z = 5090648
01
XDOT = -411
795024 XDOT = -217
359883
YDOT = 24536
164495 feet/sec YDOT = 7476
705745 meter/sec
ZDOT = 5556
006992 ZDOT = 1692
638406
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6784396
28 X = 2067883
99
Y = -12979564
40 feet Y = -3956171
23 meter
Z = 16723072
74 Z = 5097192
57
XDOT = 17127
084834 XDOT = 5220
335457
YDOT = 16106
306013 feet/sec YDOT = 4909
202073 meter/sec
ZDOT = 5551
033668 ZDOT = 1691
955062
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 15128
56028240
00016717 00000-0 10270-3 0 9001
2 25544 51
6433 281
9299 0006843 285
2810 74
7587 15
55663545 21872
Satellite: ISS
Catalog Number: 25544
Epoch time: 15128
56028240 = yrday
fracday
Element set: 900
Inclination: 51
6433 deg
RA of node: 281
9299 deg
Eccentricity:
0006843
Arg of perigee: 285
2810 deg
Mean anomaly: 74
7587 deg
Mean motion: 15
55663545 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2187
Checksum: 327
Coasting Arc #2 (Orbit 2201)
---------------------------------------
Vector Time (GMT): 2015/129/12:13:12
993
Vector Time (MET): N/A
Weight (LBS) : 911686
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4076003
53 A = 6772980
08 meter
Y = -1370958
57 meter E =
0008155
Z = -5239575
58 I = 51
26374
XDOT = 1484
661541 Wp = 85
75220
YDOT = -7477
196689 meter/sec RA = 276
38223 deg
ZDOT = 803
161934 TA = 191
95770
MA = 191
97707
Ha = 216
938 n
mi
Hp = 214
513
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13372715
01 X = -4034918
09
Y = -4497895
57 feet Y = -1416309
20 meter
Z = -17190208
61 Z = -5259276
44
XDOT = 4870
936813 XDOT = 1564
261498
YDOT = -24531
485199 feet/sec YDOT = -7460
149191 meter/sec
ZDOT = 2635
045715 ZDOT = 810
567281
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12040080
23 X = -3669816
45
Y = 7155137
71 feet Y = 2180885
98 meter
Z = -17274383
22 Z = -5265232
00
XDOT = -14966
160225 XDOT = -4561
685636
YDOT = -18755
372693 feet/sec YDOT = -5716
637597 meter/sec
ZDOT = 2668
174690 ZDOT = 813
259646
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 15129
52385437
00016717 00000-0 10270-3 0 9013
2 25544 51
6442 277
1167 0006699 289
0967 70
9461 15
55705799 22022
Satellite: ISS
Catalog Number: 25544
Epoch time: 15129
52385437 = yrday
fracday
Element set: 901
Inclination: 51
6442 deg
RA of node: 277
1167 deg
Eccentricity:
0006699
Arg of perigee: 289
0967 deg
Mean anomaly: 70
9461 deg
Mean motion: 15
55705799 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2202
Checksum: 339
Coasting Arc #3 (Orbit 2217)
---------------------------------------
Vector Time (GMT): 2015/130/12:13:12
993
Vector Time (MET): N/A
Weight (LBS) : 911686
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3506519
49 A = 6776180
14 meter
Y = 3684264
09 meter E =
0006327
Z = 4478831
00 I = 51
27136
XDOT = -2698
403817 Wp = 19
34547
YDOT = 6437
479577 meter/sec RA = 271
34286 deg
ZDOT = -3175
671140 TA = 102
75176
MA = 102
68104
Ha = 217
246 n
mi
Hp = 214
623
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11504329
05 X = 3443303
94
Y = 12087480
59 feet Y = 3723122
72 meter
Z = 14694327
42 Z = 4495711
64
XDOT = -8853
030897 XDOT = -2754
762372
YDOT = 21120
339820 feet/sec YDOT = 6406
989214 meter/sec
ZDOT = -10418
868570 ZDOT = -3188
916296
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16587207
25 X = 5055780
77
Y = -1099985
75 feet Y = -335275
66 meter
Z = 14765995
37 Z = 4500675
39
XDOT = 10608
237780 XDOT = 3233
390875
YDOT = 19013
967278 feet/sec YDOT = 5795
457226 meter/sec
ZDOT = -10476
821274 ZDOT = -3193
335124
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 15130
55164270
00016717 00000-0 10270-3 0 9029
2 25544 51
6438 271
9799 0006726 293
0383 67
0061 15
55693501 22185
Satellite: ISS
Catalog Number: 25544
Epoch time: 15130
55164270 = yrday
fracday
Element set: 902
Inclination: 51
6438 deg
RA of node: 271
9799 deg
Eccentricity:
0006726
Arg of perigee: 293
0383 deg
Mean anomaly: 67
0061 deg
Mean motion: 15
55693501 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2218
Checksum: 308
Coasting Arc #4 (Orbit 2232)
---------------------------------------
Vector Time (GMT): 2015/131/12:13:12
993
Vector Time (MET): N/A
Weight (LBS) : 911686
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2700393
49 A = 6780943
88 meter
Y = -5486063
30 meter E =
0005367
Z = -2923022
31 I = 51
28886
XDOT = 3717
990687 Wp = 339
23140
YDOT = -4487
008220 meter/sec RA = 266
32008 deg
ZDOT = 4988
721815 TA = 347
21499
MA = 347
22859
Ha = 217
356 n
mi
Hp = 214
399
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8859558
70 X = -2624647
28
Y = -17998895
33 feet Y = -5515837
32 meter
Z = -9589968
22 Z = -2935956
45
XDOT = 12198
132176 XDOT = 3743
655650
YDOT = -14721
155577 feet/sec YDOT = -4445
287753 meter/sec
ZDOT = 16367
197557 ZDOT = 5006
845517
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19558838
20 X = -5961533
88
Y = -4342445
64 feet Y = -1323577
43 meter
Z = -9644403
47 Z = -2939614
18
XDOT = -4285
756549 XDOT = -1306
298596
YDOT = -17206
444475 feet/sec YDOT = -5244
524276 meter/sec
ZDOT = 16445
693437 ZDOT = 5012
647360
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 15131
51517132
00016717 00000-0 10270-3 0 9036
2 25544 51
6446 267
1653 0006886 297
7678 62
2777 15
55750391 22334
Satellite: ISS
Catalog Number: 25544
Epoch time: 15131
51517132 = yrday
fracday
Element set: 903
Inclination: 51
6446 deg
RA of node: 267
1653 deg
Eccentricity:
0006886
Arg of perigee: 297
7678 deg
Mean anomaly: 62
2777 deg
Mean motion: 15
55750391 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2233
Checksum: 324
Coasting Arc #5 (Orbit 2248)
---------------------------------------
Vector Time (GMT): 2015/132/12:13:12
993
Vector Time (MET): N/A
Weight (LBS) : 911686
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1661782
26 A = 6784201
76 meter
Y = 6522588
98 meter E =
0006510
Z = 820857
82 I = 51
30271
XDOT = -4501
860779 Wp = 131
06064
YDOT = 1894
367445 meter/sec RA = 261
31298 deg
ZDOT = -5912
486873 TA = 40
01628
MA = 39
96833
Ha = 217
571 n
mi
Hp = 214
210
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5452041
54 X = 1584734
16
Y = 21399570
14 feet Y = 6540741
32 meter
Z = 2693103
08 Z = 828743
32
XDOT = -14769
884444 XDOT = -4493
988566
YDOT = 6215
116291 feet/sec YDOT = 1844
068679 meter/sec
ZDOT = -19397
922811 ZDOT = -5934
337114
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20273640
56 X = 6179405
64
Y = 8744660
43 feet Y = 2665372
50 meter
Z = 2725724
87 Z = 830800
94
XDOT = -3371
134831 XDOT = -1027
521897
YDOT = 13918
089691 feet/sec YDOT = 4242
233738 meter/sec
ZDOT = -19491
917591 ZDOT = -5941
136482
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 15132
54291408
00016717 00000-0 10270-3 0 9046
2 25544 51
6442 262
0290 0006926 301
5996 58
4481 15
55792479 22492
Satellite: ISS
Catalog Number: 25544
Epoch time: 15132
54291408 = yrday
fracday
Element set: 904
Inclination: 51
6442 deg
RA of node: 262
0290 deg
Eccentricity:
0006926
Arg of perigee: 301
5996 deg
Mean anomaly: 58
4481 deg
Mean motion: 15
55792479 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2249
Checksum: 322
Coasting Arc #6 (Orbit 2264)
---------------------------------------
Vector Time (GMT): 2015/133/12:13:12
993
Vector Time (MET): N/A
Weight (LBS) : 911686
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -430971
95 A = 6783515
91 meter
Y = -6608625
52 meter E =
0012654
Z = 1429775
85 I = 51
30753
XDOT = 4979
195256 Wp = 31
20021
YDOT = 925
570039 meter/sec RA = 256
31147 deg
ZDOT = 5766
680539 TA = 344
48625
MA = 344
52500
Ha = 217
673 n
mi
Hp = 213
967
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1413949
97 X = -363986
09
Y = -21681842
26 feet Y = -6613070
38 meter
Z = 4690865
67 Z = 1427845
03
XDOT = 16335
942442 XDOT = 4940
462538
YDOT = 3036
647108 feet/sec YDOT = 981
034151 meter/sec
ZDOT = 18919
555573 ZDOT = 5790
774701
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18267747
82 X = -5568009
53
Y = -11766794
09 feet Y = -3586518
84 meter
Z = 4683770
44 Z = 1427613
23
XDOT = 11248
552329 XDOT = 3428
558750
YDOT = -9875
137427 feet/sec YDOT = -3009
941888 meter/sec
ZDOT = 19022
664404 ZDOT = 5798
108110
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 15133
57063372
00016717 00000-0 10270-3 0 9058
2 25544 51
6453 256
8926 0006921 306
4848 53
5667 15
55833399 22653
Satellite: ISS
Catalog Number: 25544
Epoch time: 15133
57063372 = yrday
fracday
Element set: 905
Inclination: 51
6453 deg
RA of node: 256
8926 deg
Eccentricity:
0006921
Arg of perigee: 306
4848 deg
Mean anomaly: 53
5667 deg
Mean motion: 15
55833399 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2265
Checksum: 335
Coasting Arc #7 (Orbit 2279)
---------------------------------------
Vector Time (GMT): 2015/134/12:13:12
993
Vector Time (MET): N/A
Weight (LBS) : 911686
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -954505
98 A = 6779285
09 meter
Y = 5767653
93 meter E =
0004639
Z = -3436779
84 I = 51
30212
XDOT = -5047
686707 Wp = 354
57692
YDOT = -3548
583022 meter/sec RA = 251
30146 deg
ZDOT = -4548
333937 TA = 225
91589
MA = 225
95409
Ha = 217
864 n
mi
Hp = 213
744
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3131581
28 X = -1002235
46
Y = 18922749
11 feet Y = 5756713
13 meter
Z = -11275524
40 Z = -3441532
69
XDOT = -16560
651927 XDOT = -4985
535998
YDOT = -11642
332750 feet/sec YDOT = -3604
682081 meter/sec
ZDOT = -14922
355435 ZDOT = -4572
704021
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13601495
61 X = 4145735
86
Y = 13505317
60 feet Y = 4116420
80 meter
Z = -11296919
91 Z = -3443301
19
XDOT = -18068
884460 XDOT = -5507
395983
YDOT = 5614
654532 feet/sec YDOT = 1711
346701 meter/sec
ZDOT = -15026
186788 ZDOT = -4579
981733
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 15134
53410092
00016717 00000-0 10270-3 0 9061
2 25544 51
6454 252
0776 0007015 309
9036 50
1500 15
55853851 22808
Satellite: ISS
Catalog Number: 25544
Epoch time: 15134
53410092 = yrday
fracday
Element set: 906
Inclination: 51
6454 deg
RA of node: 252
0776 deg
Eccentricity:
0007015
Arg of perigee: 309
9036 deg
Mean anomaly: 50
1500 deg
Mean motion: 15
55853851 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2280
Checksum: 283
Coasting Arc #8 (Orbit 2295)
---------------------------------------
Vector Time (GMT): 2015/135/12:13:12
993
Vector Time (MET): N/A
Weight (LBS) : 911686
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2394325
98 A = 6774220
84 meter
Y = -4126233
30 meter E =
0001796
Z = 4807965
00 I = 51
29767
XDOT = 4632
779814 Wp = 40
45211
YDOT = 5586
346864 meter/sec RA = 246
27349 deg
ZDOT = 2487
981849 TA = 24
99866
MA = 24
98996
Ha = 217
857 n
mi
Hp = 213
496
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7855400
20 X = 2416932
81
Y = -13537510
84 feet Y = -4099332
01 meter
Z = 15774163
37 Z = 4819651
27
XDOT = 15199
408840 XDOT = 4557
881717
YDOT = 18327
909658 feet/sec YDOT = 5637
734841 meter/sec
ZDOT = 8162
670107 ZDOT = 2510
305536
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6732202
13 X = -2051975
21
Y = -14072776
00 feet Y = -4289382
13 meter
Z = 15824985
70 Z = 4823455
64
XDOT = 22662
961377 XDOT = 6907
670628
YDOT = -1559
123797 feet/sec YDOT = -475
220933 meter/sec
ZDOT = 8257
378227 ZDOT = 2516
848884
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 15135
56177592
00016717 00000-0 10270-3 0 9071
2 25544 51
6461 246
9409 0007094 314
3435 45
7136 15
55922792 22964
Satellite: ISS
Catalog Number: 25544
Epoch time: 15135
56177592 = yrday
fracday
Element set: 907
Inclination: 51
6461 deg
RA of node: 246
9409 deg
Eccentricity:
0007094
Arg of perigee: 314
3435 deg
Mean anomaly: 45
7136 deg
Mean motion: 15
55922792 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2296
Checksum: 329
Coasting Arc #9 (Orbit 2303)
---------------------------------------
Vector Time (GMT): 2015/136/01:18:39
961
Vector Time (MET): N/A
Weight (LBS) : 911145
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1981770
74 A = 6777639
44 meter
Y = 4468254
02 meter E =
0006686
Z = -4700539
29 I = 51
30502
XDOT = -5004
022269 Wp = 29
40709
YDOT = -5114
217623 meter/sec RA = 243
53888 deg
ZDOT = -2747
715700 TA = 213
22834
MA = 213
27034
Ha = 218
322 n
mi
Hp = 216
185
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6501872
50 X = -2008754
61
Y = 14659626
06 feet Y = 4445941
77 meter
Z = -15421716
84 Z = -4710232
02
XDOT = -16417
395895 XDOT = -4933
114310
YDOT = -16778
929209 feet/sec YDOT = -5169
779358 meter/sec
ZDOT = -9014
815289 ZDOT = -2771
852616
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12012712
79 X = -3661474
86
Y = -10562486
30 feet Y = -3219445
82 meter
Z = -15464053
39 Z = -4713443
47
XDOT = 20193
729231 XDOT = 6155
048670
YDOT = -9598
560488 feet/sec YDOT = -2925
641237 meter/sec
ZDOT = -9117
384562 ZDOT = -2778
978815
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 15136
07561979
00016717 00000-0 10270-3 0 9085
2 25544 51
6448 244
3755 0007364 287
9817 72
0533 15
54909355 23047
Satellite: ISS
Catalog Number: 25544
Epoch time: 15136
07561979 = yrday
fracday
Element set: 908
Inclination: 51
6448 deg
RA of node: 244
3755 deg
Eccentricity:
0007364
Arg of perigee: 287
9817 deg
Mean anomaly: 72
0533 deg
Mean motion: 15
54909355 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2304
Checksum: 336
Coasting Arc #10 (Orbit 2319)
---------------------------------------
Vector Time (GMT): 2015/137/01:18:39
961
Vector Time (MET): N/A
Weight (LBS) : 911145
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3229474
44 A = 6775106
45 meter
Y = -2795830
77 meter E =
0004544
Z = 5262492
88 I = 51
31178
XDOT = 4404
729942 Wp = 288
68982
YDOT = 6245
202380 meter/sec RA = 238
50995 deg
ZDOT = 616
703655 TA = 155
40630
MA = 155
38463
Ha = 218
413 n
mi
Hp = 216
177
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10595388
58 X = 3234934
30
Y = -9172673
12 feet Y = -2759686
34 meter
Z = 17265396
60 Z = 5278194
54
XDOT = 14451
213722 XDOT = 4331
571450
YDOT = 20489
509122 feet/sec YDOT = 6294
049875 meter/sec
ZDOT = 2023
305956 ZDOT = 637
923965
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5762395
47 X = 1756378
14
Y = 12682627
87 feet Y = 3865664
97 meter
Z = 17333201
08 Z = 5283159
69
XDOT = -22855
073888 XDOT = -6966
226521
YDOT = 7504
562471 feet/sec YDOT = 2287
390641 meter/sec
ZDOT = 2113
183588 ZDOT = 644
098358
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 15137
10393766
00016717 00000-0 10270-3 0 9098
2 25544 51
6447 239
2431 0007494 291
4004 68
6349 15
54945955 23202
Satellite: ISS
Catalog Number: 25544
Epoch time: 15137
10393766 = yrday
fracday
Element set: 909
Inclination: 51
6447 deg
RA of node: 239
2431 deg
Eccentricity:
0007494
Arg of perigee: 291
4004 deg
Mean anomaly: 68
6349 deg
Mean motion: 15
54945955 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2320
Checksum: 324
Coasting Arc #11 (Orbit 2334)
---------------------------------------
Vector Time (GMT): 2015/138/01:18:39
961
Vector Time (MET): N/A
Weight (LBS) : 911145
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4361578
18 A = 6775755
77 meter
Y = 967687
39 meter E =
0006552
Z = -5099788
22 I = 51
33198
XDOT = -3361
507949 Wp = 86
15438
YDOT = -6698
941464 meter/sec RA = 233
47925 deg
ZDOT = 1606
010761 TA = 199
39914
MA = 199
42408
Ha = 218
611 n
mi
Hp = 215
781
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14309639
71 X = -4347301
57
Y = 3174827
40 feet Y = 918993
49 meter
Z = -16731588
65 Z = -5120941
62
XDOT = -11028
569387 XDOT = -3294
150508
YDOT = -21978
154409 feet/sec YDOT = -6736
155518 meter/sec
ZDOT = 5269
064175 ZDOT = 1589
844099
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 802146
88 X = 244494
37
Y = -14531105
46 feet Y = -4429080
94 meter
Z = -16822452
58 Z = -5127483
55
XDOT = 23095
850202 XDOT = 7039
615141
YDOT = -4737
711792 feet/sec YDOT = -1444
054554 meter/sec
ZDOT = 5200
921816 ZDOT = 1585
240970
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 15138
06796812
00016717 00000-0 10270-3 0 9105
2 25544 51
6452 234
4316 0007514 296
0245 64
0134 15
54961272 23356
Satellite: ISS
Catalog Number: 25544
Epoch time: 15138
06796812 = yrday
fracday
Element set: 910
Inclination: 51
6452 deg
RA of node: 234
4316 deg
Eccentricity:
0007514
Arg of perigee: 296
0245 deg
Mean anomaly: 64
0134 deg
Mean motion: 15
54961272 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2335
Checksum: 295
Coasting Arc #12 (Orbit 2350)
---------------------------------------
Vector Time (GMT): 2015/139/01:18:39
961
Vector Time (MET): N/A
Weight (LBS) : 911145
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5244658
40 A = 6779136
46 meter
Y = 839538
24 meter E =
0007346
Z = 4214220
99 I = 51
36293
XDOT = 1880
051981 Wp = 25
06618
YDOT = 6489
534890 meter/sec RA = 228
45692 deg
ZDOT = -3623
710617 TA = 102
21059
MA = 102
12831
Ha = 218
867 n
mi
Hp = 215
617
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17206884
50 X = 5214409
22
Y = 2754390
56 feet Y = 898017
99 meter
Z = 13826184
35 Z = 4239625
56
XDOT = 6168
149543 XDOT = 1824
947658
YDOT = 21291
124968 feet/sec YDOT = 6510
251029 meter/sec
ZDOT = -11888
814360 ZDOT = -3614
710883
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7028391
46 X = -2142253
72
Y = 15850715
90 feet Y = 4831298
21 meter
Z = 13934971
63 Z = 4247379
35
XDOT = -21022
401842 XDOT = -6407
628081
YDOT = 1122
750961 feet/sec YDOT = 342
214493 meter/sec
ZDOT = -11851
355645 ZDOT = -3612
293201
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 15139
09624629
00016717 00000-0 10270-3 0 9116
2 25544 51
6447 229
2994 0007592 300
6943 59
3461 15
55002552 23513
Satellite: ISS
Catalog Number: 25544
Epoch time: 15139
09624629 = yrday
fracday
Element set: 911
Inclination: 51
6447 deg
RA of node: 229
2994 deg
Eccentricity:
0007592
Arg of perigee: 300
6943 deg
Mean anomaly: 59
3461 deg
Mean motion: 15
55002552 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2351
Checksum: 313
Coasting Arc #13 (Orbit 2365)
---------------------------------------
Vector Time (GMT): 2015/140/01:18:39
961
Vector Time (MET): N/A
Weight (LBS) : 911145
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5716287
02 A = 6783489
92 meter
Y = -2406980
74 meter E =
0007151
Z = -2735344
75 I = 51
39933
XDOT = -55
858073 Wp = 341
81052
YDOT = -5698
817078 meter/sec RA = 223
44846 deg
ZDOT = 5134
466977 TA = 347
10324
MA = 347
12152
Ha = 218
948 n
mi
Hp = 215
438
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18754222
51 X = -5675659
28
Y = -7896918
43 feet Y = -2470676
59 meter
Z = -8974228
17 Z = -2763015
27
XDOT = -183
261395 XDOT = -17
070048
YDOT = -18696
906423 feet/sec YDOT = -5699
225294 meter/sec
ZDOT = 16845
364099 ZDOT = 5134
289338
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12124693
69 X = 3695606
64
Y = -16276905
64 feet Y = -4961200
84 meter
Z = -9092474
90 Z = -2771386
35
XDOT = 17039
263442 XDOT = 5193
567497
YDOT = 3287
909714 feet/sec YDOT = 1002
154881 meter/sec
ZDOT = 16845
592275 ZDOT = 5134
536525
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 15140
06023867
00016717 00000-0 10270-3 0 9123
2 25544 51
6448 224
4872 0007683 304
2773 55
7652 15
55014923 23661
Satellite: ISS
Catalog Number: 25544
Epoch time: 15140
06023867 = yrday
fracday
Element set: 912
Inclination: 51
6448 deg
RA of node: 224
4872 deg
Eccentricity:
0007683
Arg of perigee: 304
2773 deg
Mean anomaly: 55
7652 deg
Mean motion: 15
55014923 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2366
Checksum: 308
Coasting Arc #14 (Orbit 2381)
---------------------------------------
Vector Time (GMT): 2015/141/01:18:39
961
Vector Time (MET): N/A
Weight (LBS) : 911145
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5663562
06 A = 6786445
66 meter
Y = 3637147
79 meter E =
0005897
Z = 845150
81 I = 51
43221
XDOT = -1975
141847 Wp = 123
44710
YDOT = 4456
820695 meter/sec RA = 218
45473 deg
ZDOT = -5917
543496 TA = 47
38420
MA = 47
33449
Ha = 219
199 n
mi
Hp = 215
264
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18581240
36 X = 5618364
21
Y = 11932899
56 feet Y = 3700228
65 meter
Z = 2772804
48 Z = 872554
12
XDOT = -6480
124169 XDOT = -1996
086789
YDOT = 14622
115141 feet/sec YDOT = 4434
616799 meter/sec
ZDOT = -19414
512781 ZDOT = -5927
188914
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15748497
41 X = -4800142
01
Y = 15458959
69 feet Y = 4711890
91 meter
Z = 2889710
10 Z = 880783
64
XDOT = -11721
877131 XDOT = -3572
828150
YDOT = -8288
722474 feet/sec YDOT = -2526
402610 meter/sec
ZDOT = -19456
652907 ZDOT = -5930
387806
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 15141
08847886
00016717 00000-0 10270-3 0 9132
2 25544 51
6443 219
3547 0007550 307
5596 52
4871 15
55006869 23825
Satellite: ISS
Catalog Number: 25544
Epoch time: 15141
08847886 = yrday
fracday
Element set: 913
Inclination: 51
6443 deg
RA of node: 219
3547 deg
Eccentricity:
0007550
Arg of perigee: 307
5596 deg
Mean anomaly: 52
4871 deg
Mean motion: 15
55006869 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2382
Checksum: 331
Coasting Arc #15 (Orbit 2397)
---------------------------------------
Vector Time (GMT): 2015/142/01:18:39
961
Vector Time (MET): N/A
Weight (LBS) : 911145
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5002625
57 A = 6786018
16 meter
Y = -4420391
93 meter E =
0013820
Z = 1165980
70 I = 51
45630
XDOT = 3982
392060 Wp = 24
75084
YDOT = -2959
142801 meter/sec RA = 213
46579 deg
ZDOT = 5855
044664 TA = 347
95701
MA = 347
99002
Ha = 219
337 n
mi
Hp = 214
999
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16412813
55 X = -4958487
82
Y = -14502598
21 feet Y = -4476087
88 meter
Z = 3825395
99 Z = 1141785
58
XDOT = 13065
590747 XDOT = 3986
744118
YDOT = -9708
473757 feet/sec YDOT = -2914
585258 meter/sec
ZDOT = 19209
464120 ZDOT = 5874
400800
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17559672
06 X = 5352188
04
Y = -13120264
98 feet Y = -3999056
77 meter
Z = 3722367
80 Z = 1134577
71
XDOT = 5895
027968 XDOT = 1796
804525
YDOT = 13375
615155 feet/sec YDOT = 4076
887499 meter/sec
ZDOT = 19293
003119 ZDOT = 5880
507351
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 15142
11669631
00016717 00000-0 10270-3 0 9148
2 25544 51
6438 214
2208 0007813 312
1264 47
9225 15
55081804 23984
Satellite: ISS
Catalog Number: 25544
Epoch time: 15142
11669631 = yrday
fracday
Element set: 914
Inclination: 51
6438 deg
RA of node: 214
2208 deg
Eccentricity:
0007813
Arg of perigee: 312
1264 deg
Mean anomaly: 47
9225 deg
Mean motion: 15
55081804 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2398
Checksum: 296
Coasting Arc #16 (Orbit 2412)
---------------------------------------
Vector Time (GMT): 2015/143/01:18:39
961
Vector Time (MET): N/A
Weight (LBS) : 911145
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3751117
38 A = 6782741
99 meter
Y = 4775224
80 meter E =
0004194
Z = -3025761
31 I = 51
47158
XDOT = -5712
019267 Wp = 341
90149
YDOT = 1362
900916 meter/sec RA = 208
47348 deg
ZDOT = -4924
680534 TA = 232
85529
MA = 232
89361
Ha = 219
489 n
mi
Hp = 214
876
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12306815
54 X = 3712138
96
Y = 15666748
04 feet Y = 4816954
53 meter
Z = -9927038
41 Z = -3007633
35
XDOT = -18740
220693 XDOT = -5702
912659
YDOT = 4471
459697 feet/sec YDOT = 1299
076662 meter/sec
ZDOT = -16157
088366 ZDOT = -4952
406324
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17710351
02 X = -5398114
99
Y = 9207070
36 feet Y = 2806315
05 meter
Z = -9850082
05 Z = -3002305
01
XDOT = -218
482658 XDOT = -66
593514
YDOT = -17853
579587 feet/sec YDOT = -5441
771058 meter/sec
ZDOT = -16276
269367 ZDOT = -4961
006903
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 15143
08063449
00016717 00000-0 10270-3 0 9151
2 25544 51
6431 209
4087 0007870 315
0227 45
0288 15
55079656 24130
Satellite: ISS
Catalog Number: 25544
Epoch time: 15143
08063449 = yrday
fracday
Element set: 915
Inclination: 51
6431 deg
RA of node: 209
4087 deg
Eccentricity:
0007870
Arg of perigee: 315
0227 deg
Mean anomaly: 45
0288 deg
Mean motion: 15
55079656 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2413
Checksum: 305
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