[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
September 3rd 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 24756 99 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 121 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 049 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
256/03:26:12
497 1
3 1
5 1
5
N/A 0
5 0
0 227
8
000/00:03:20
994 -0
4 0
0 219
8
Coasting Arc #1 (Orbit 669)
---------------------------------------
Vector Time (GMT): 2013/245/12:22:38
082
Vector Time (MET): N/A
Weight (LBS) : 957467
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4102238
22 A = 6790165
49 meter
Y = 2229415
52 meter E =
0012793
Z = -4941384
36 I = 51
98599
XDOT = -1115
897358 Wp = 90
90537
YDOT = 7203
815788 meter/sec RA = 84
34472 deg
ZDOT = 2328
771541 TA = 201
78855
MA = 201
84301
Ha = 227
739 n
mi
Hp = 220
184
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13458786
82 X = 4101007
10
Y = 7314355
37 feet Y = 2275282
12 meter
Z = -16211890
96 Z = -4921459
48
XDOT = -3661
080571 XDOT = -1207
681453
YDOT = 23634
566232 feet/sec YDOT = 7190
824083 meter/sec
ZDOT = 7640
326577 ZDOT = 2323
127250
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11505311
15 X = -3506818
84
Y = -10245057
53 feet Y = -3122693
53 meter
Z = -16128569
59 Z = -4915988
01
XDOT = 8316
077587 XDOT = 2534
740448
YDOT = -21302
201367 feet/sec YDOT = -6492
910977 meter/sec
ZDOT = 7615
644120 ZDOT = 2321
248328
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 13245
52777349
00016717 00000-0 10270-3 0 9006
2 25544 51
6455 85
0946 0003507 20
9791 339
1503 15
50347674 6702
Satellite: ISS
Catalog Number: 25544
Epoch time: 13245
52777349 = yrday
fracday
Element set: 900
Inclination: 51
6455 deg
RA of node: 85
0946 deg
Eccentricity:
0003507
Arg of perigee: 20
9791 deg
Mean anomaly: 339
1503 deg
Mean motion: 15
50347674 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 670
Checksum: 312
Coasting Arc #2 (Orbit 685)
---------------------------------------
Vector Time (GMT): 2013/246/12:22:38
082
Vector Time (MET): N/A
Weight (LBS) : 957467
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4216983
65 A = 6790948
14 meter
Y = -2431542
90 meter E =
0010817
Z = 4730955
14 I = 51
98484
XDOT = 912
657992 Wp = 51
18314
YDOT = -7072
135010 meter/sec RA = 79
40917 deg
ZDOT = -2810
406098 TA = 66
61050
MA = 66
49677
Ha = 227
812 n
mi
Hp = 220
037
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13835248
18 X = -4212461
59
Y = -7977502
96 feet Y = -2478674
19 meter
Z = 15521506
37 Z = 4710480
88
XDOT = 2994
284751 XDOT = 1005
324338
YDOT = -23202
542683 feet/sec YDOT = -7061
411209 meter/sec
ZDOT = -9220
492447 ZDOT = -2805
746844
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11901443
73 X = 3627560
05
Y = 10773123
58 feet Y = 3283648
07 meter
Z = 15435907
85 Z = 4704864
71
XDOT = -7161
187276 XDOT = -2182
729882
YDOT = 21144
646868 feet/sec YDOT = 6444
888365 meter/sec
ZDOT = -9199
956344 ZDOT = -2804
146694
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 13246
55911243
00016717 00000-0 10270-3 0 9014
2 25544 51
6456 79
9826 0003488 22
7759 337
3546 15
50361938 6867
Satellite: ISS
Catalog Number: 25544
Epoch time: 13246
55911243 = yrday
fracday
Element set: 901
Inclination: 51
6456 deg
RA of node: 79
9826 deg
Eccentricity:
0003488
Arg of perigee: 22
7759 deg
Mean anomaly: 337
3546 deg
Mean motion: 15
50361938 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 686
Checksum: 335
Coasting Arc #3 (Orbit 700)
---------------------------------------
Vector Time (GMT): 2013/247/12:22:38
082
Vector Time (MET): N/A
Weight (LBS) : 957467
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4378632
92 A = 6791739
33 meter
Y = 2588462
30 meter E =
0010493
Z = -4509730
35 I = 51
98036
XDOT = -726
953609 Wp = 91
09516
YDOT = 6889
279551 meter/sec RA = 74
47233 deg
ZDOT = 3254
776030 TA = 211
54188
MA = 211
60482
Ha = 227
782 n
mi
Hp = 219
958
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14365593
56 X = 4371269
55
Y = 8492330
39 feet Y = 2637385
31 meter
Z = -14795703
24 Z = -4488477
74
XDOT = -2385
018402 XDOT = -819
747661
YDOT = 22602
623198 feet/sec YDOT = 6880
631797 meter/sec
ZDOT = 10678
399050 ZDOT = 3251
018476
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12498971
61 X = -3809686
55
Y = -11175272
00 feet Y = -3406222
91 meter
Z = -14706862
10 Z = -4482651
57
XDOT = 6045
350220 XDOT = 1842
622747
YDOT = -20764
831727 feet/sec YDOT = -6329
120710 meter/sec
ZDOT = 10661
667007 ZDOT = 3249
676104
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 13247
52597764
00016717 00000-0 10270-3 0 9021
2 25544 51
6447 75
1886 0003499 28
7807 331
3536 15
50394058 7013
Satellite: ISS
Catalog Number: 25544
Epoch time: 13247
52597764 = yrday
fracday
Element set: 902
Inclination: 51
6447 deg
RA of node: 75
1886 deg
Eccentricity:
0003499
Arg of perigee: 28
7807 deg
Mean anomaly: 331
3536 deg
Mean motion: 15
50394058 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 701
Checksum: 328
Coasting Arc #4 (Orbit 716)
---------------------------------------
Vector Time (GMT): 2013/248/12:22:38
082
Vector Time (MET): N/A
Weight (LBS) : 957467
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4549229
27 A = 6792755
98 meter
Y = -2758669
41 meter E =
0012945
Z = 4217003
24 I = 51
97467
XDOT = 601
432252 Wp = 64
05589
YDOT = -6681
269997 meter/sec RA = 69
53646 deg
ZDOT = -3707
587934 TA = 63
89481
MA = 63
76166
Ha = 227
834 n
mi
Hp = 219
828
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14925292
89 X = -4538528
02
Y = -9050752
65 feet Y = -2809481
44 meter
Z = 13835312
48 Z = 4194929
99
XDOT = 1973
202927 XDOT = 694
109295
YDOT = -21920
177154 feet/sec YDOT = -6674
026652 meter/sec
ZDOT = -12164
002408 ZDOT = -3704
440354
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13133309
47 X = 4003032
73
Y = 11607798
28 feet Y = 3538056
92 meter
Z = 13743055
12 Z = 4188883
20
XDOT = -5120
927787 XDOT = -1560
858789
YDOT = 20234
804340 feet/sec YDOT = 6167
568363 meter/sec
ZDOT = -12149
853189 ZDOT = -3703
275252
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 13248
55728283
00016717 00000-0 10270-3 0 9038
2 25544 51
6447 70
0759 0003483 30
6692 329
4661 15
50407794 7179
Satellite: ISS
Catalog Number: 25544
Epoch time: 13248
55728283 = yrday
fracday
Element set: 903
Inclination: 51
6447 deg
RA of node: 70
0759 deg
Eccentricity:
0003483
Arg of perigee: 30
6692 deg
Mean anomaly: 329
4661 deg
Mean motion: 15
50407794 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 717
Checksum: 321
Coasting Arc #5 (Orbit 731)
---------------------------------------
Vector Time (GMT): 2013/249/12:22:38
082
Vector Time (MET): N/A
Weight (LBS) : 957467
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4755590
17 A = 6793679
40 meter
Y = 2868952
85 meter E =
0008351
Z = -3918700
19 I = 51
96677
XDOT = -503
169411 Wp = 82
11770
YDOT = 6438
329099 meter/sec RA = 64
59985 deg
ZDOT = 4111
594268 TA = 230
83339
MA = 230
90761
Ha = 227
819 n
mi
Hp = 219
721
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15602329
96 X = 4742191
38
Y = 9412574
96 feet Y = 2922057
47 meter
Z = -12856627
92 Z = -3895630
96
XDOT = -1650
818277 XDOT = -595
099753
YDOT = 21123
126966 feet/sec YDOT = 6432
188839 meter/sec
ZDOT = 13489
482505 ZDOT = 4108
925832
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13933855
77 X = -4247039
24
Y = -11846805
45 feet Y = -3610906
30 meter
Z = -12760212
11 Z = -3889312
65
XDOT = 4297
967976 XDOT = 1310
020639
YDOT = -19541
008621 feet/sec YDOT = -5956
099428 meter/sec
ZDOT = 13477
371142 ZDOT = 4107
902724
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 13249
52411602
00016717 00000-0 10270-3 0 9041
2 25544 51
6450 65
2821 0003522 36
8270 323
3122 15
50444465 7321
Satellite: ISS
Catalog Number: 25544
Epoch time: 13249
52411602 = yrday
fracday
Element set: 904
Inclination: 51
6450 deg
RA of node: 65
2821 deg
Eccentricity:
0003522
Arg of perigee: 36
8270 deg
Mean anomaly: 323
3122 deg
Mean motion: 15
50444465 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 732
Checksum: 266
Coasting Arc #6 (Orbit 747)
---------------------------------------
Vector Time (GMT): 2013/250/12:22:38
082
Vector Time (MET): N/A
Weight (LBS) : 957467
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4961639
04 A = 6794810
81 meter
Y = -2986908
24 meter E =
0014703
Z = 3544547
30 I = 51
95639
XDOT = 479
113298 Wp = 77
58063
YDOT = -6175
506209 meter/sec RA = 59
66362 deg
ZDOT = -4514
446598 TA = 60
90109
MA = 60
75395
Ha = 227
847 n
mi
Hp = 219
616
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16278343
32 X = -4945088
47
Y = -9799567
72 feet Y = -3042299
47 meter
Z = 11629092
19 Z = 3520484
68
XDOT = 1571
894023 XDOT = 570
063512
YDOT = -20260
847143 feet/sec YDOT = -6169
640481 meter/sec
ZDOT = -14811
176503 ZDOT = -4511
897440
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14740104
69 X = 4492783
91
Y = 12086109
56 feet Y = 3683846
19 meter
Z = 11528531
71 Z = 3513896
47
XDOT = -3730
007086 XDOT = -1136
906160
YDOT = 18725
419137 feet/sec YDOT = 5707
507753 meter/sec
ZDOT = -14799
594641 ZDOT = -4510
916447
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 13250
55538663
00016717 00000-0 10270-3 0 9054
2 25544 51
6448 60
1691 0003507 38
9167 321
2235 15
50457148 7489
Satellite: ISS
Catalog Number: 25544
Epoch time: 13250
55538663 = yrday
fracday
Element set: 905
Inclination: 51
6448 deg
RA of node: 60
1691 deg
Eccentricity:
0003507
Arg of perigee: 38
9167 deg
Mean anomaly: 321
2235 deg
Mean motion: 15
50457148 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 748
Checksum: 307
Coasting Arc #7 (Orbit 762)
---------------------------------------
Vector Time (GMT): 2013/251/12:22:38
082
Vector Time (MET): N/A
Weight (LBS) : 957467
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5188365
73 A = 6795739
68 meter
Y = 3034950
53 meter E =
0007787
Z = -3172125
81 I = 51
94491
XDOT = -487
194108 Wp = 61
98061
YDOT = 5898
488558 meter/sec RA = 54
72722 deg
ZDOT = 4859
197253 TA = 261
66817
MA = 261
75647
Ha = 227
840 n
mi
Hp = 219
489
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17022197
29 X = 5169452
02
Y = 9957186
78 feet Y = 3092864
02 meter
Z = -10407236
91 Z = -3146967
40
XDOT = -1598
405866 XDOT = -576
720837
YDOT = 19351
996581 feet/sec YDOT = 5892
540422 meter/sec
ZDOT = 15942
248206 ZDOT = 4856
612375
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15655497
42 X = -4771795
62
Y = -12082368
35 feet Y = -3682705
87 meter
Z = -10302093
22 Z = -3140078
01
XDOT = 3304
742133 XDOT = 1007
285402
YDOT = -17829
589827 feet/sec YDOT = -5434
458979 meter/sec
ZDOT = 15930
546913 ZDOT = 4855
630699
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 13251
52218675
00016717 00000-0 10270-3 0 9061
2 25544 51
6461 55
3759 0003574 44
2127 315
9309 15
50497810 7634
Satellite: ISS
Catalog Number: 25544
Epoch time: 13251
52218675 = yrday
fracday
Element set: 906
Inclination: 51
6461 deg
RA of node: 55
3759 deg
Eccentricity:
0003574
Arg of perigee: 44
2127 deg
Mean anomaly: 315
9309 deg
Mean motion: 15
50497810 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 763
Checksum: 309
Coasting Arc #8 (Orbit 778)
---------------------------------------
Vector Time (GMT): 2013/252/12:22:38
082
Vector Time (MET): N/A
Weight (LBS) : 957467
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5401710
31 A = 6796812
29 meter
Y = -3087767
01 meter E =
0015791
Z = 2721688
66 I = 51
92965
XDOT = 579
481287 Wp = 90
86289
YDOT = -5610
490282 meter/sec RA = 49
79041 deg
ZDOT = -5189
296633 TA = 58
53524
MA = 58
38099
Ha = 227
831 n
mi
Hp = 219
410
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17722146
70 X = -5380002
06
Y = -10130469
19 feet Y = -3148050
72 meter
Z = 8929424
73 Z = 2695500
52
XDOT = 1901
185325 XDOT = 667
384297
YDOT = -18407
120347 feet/sec YDOT = -5603
519172 meter/sec
ZDOT = -17025
251422 ZDOT = -5186
267482
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16527947
74 X = 5037718
47
Y = 12061114
45 feet Y = 3676227
68 meter
Z = 8819976
03 Z = 2688328
69
XDOT = -3180
843467 XDOT = -969
521089
YDOT = 16861
604226 feet/sec YDOT = 5139
416968 meter/sec
ZDOT = -17011
717925 ZDOT = -5185
171624
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 13252
55342180
00016717 00000-0 10270-3 0 9075
2 25544 51
6457 50
2628 0003556 46
3814 313
7632 15
50512837 7793
Satellite: ISS
Catalog Number: 25544
Epoch time: 13252
55342180 = yrday
fracday
Element set: 907
Inclination: 51
6457 deg
RA of node: 50
2628 deg
Eccentricity:
0003556
Arg of perigee: 46
3814 deg
Mean anomaly: 313
7632 deg
Mean motion: 15
50512837 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 779
Checksum: 302
Coasting Arc #9 (Orbit 793)
---------------------------------------
Vector Time (GMT): 2013/253/12:22:38
082
Vector Time (MET): N/A
Weight (LBS) : 957467
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5618303
87 A = 6797608
25 meter
Y = 3066849
92 meter E =
0009626
Z = -2282029
93 I = 51
91387
XDOT = -702
902106 Wp = 45
82802
YDOT = 5331
330933 meter/sec RA = 44
85356 deg
ZDOT = 5455
081158 TA = 288
91633
MA = 289
02065
Ha = 227
837 n
mi
Hp = 219
272
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18432755
47 X = 5594677
67
Y = 10061843
57 feet Y = 3129545
07 meter
Z = -7486974
84 Z = -2254794
18
XDOT = -2306
109271 XDOT = -788
965456
YDOT = 17491
243217 feet/sec YDOT = 5322
989867 meter/sec
ZDOT = 17897
247895 ZDOT = 5451
457026
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17437944
99 X = -5315085
63
Y = -11773568
89 feet Y = -3588583
80 meter
Z = -7373134
51 Z = -2247331
40
XDOT = 3211
788457 XDOT = 978
953122
YDOT = -15911
726488 feet/sec YDOT = -4849
894234 meter/sec
ZDOT = 17881
249438 ZDOT = 5450
204829
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 13253
52018783
00016717 00000-0 10270-3 0 9083
2 25544 51
6474 45
4701 0003639 50
3985 309
7486 15
50552131 7946
Satellite: ISS
Catalog Number: 25544
Epoch time: 13253
52018783 = yrday
fracday
Element set: 908
Inclination: 51
6474 deg
RA of node: 45
4701 deg
Eccentricity:
0003639
Arg of perigee: 50
3985 deg
Mean anomaly: 309
7486 deg
Mean motion: 15
50552131 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 794
Checksum: 313
Coasting Arc #10 (Orbit 809)
---------------------------------------
Vector Time (GMT): 2013/254/12:22:38
082
Vector Time (MET): N/A
Weight (LBS) : 957467
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5805880
24 A = 6798418
38 meter
Y = -3051956
28 meter E =
0015899
Z = 1765391
83 I = 51
89370
XDOT = 914
106433 Wp = 103
26251
YDOT = -5052
674903 meter/sec RA = 39
91548 deg
ZDOT = -5689
188543 TA = 57
45071
MA = 57
29724
Ha = 227
786 n
mi
Hp = 219
212
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19048163
51 X = -5779896
93
Y = -10012979
91 feet Y = -3116735
92 meter
Z = 5791967
93 Z = 1737250
55
XDOT = 2999
036854 XDOT = 998
175294
YDOT = -16577
017398 feet/sec YDOT = -5041
983088 meter/sec
ZDOT = -18665
316741 ZDOT = -5684
543354
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18244716
63 X = 5560989
63
Y = 11470460
71 feet Y = 3496196
43 meter
Z = 5674331
54 Z = 1729536
25
XDOT = -3561
977459 XDOT = -1085
690729
YDOT = 14954
573056 feet/sec YDOT = 4558
153867 meter/sec
ZDOT = -18645
066957 ZDOT = -5683
016409
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 13254
55138606
00016717 00000-0 10270-3 0 9095
2 25544 51
6468 40
3569 0003619 52
6075 307
5403 15
50575199 8101
Satellite: ISS
Catalog Number: 25544
Epoch time: 13254
55138606 = yrday
fracday
Element set: 909
Inclination: 51
6468 deg
RA of node: 40
3569 deg
Eccentricity:
0003619
Arg of perigee: 52
6075 deg
Mean anomaly: 307
5403 deg
Mean motion: 15
50575199 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 810
Checksum: 310
Coasting Arc #11 (Orbit 824)
---------------------------------------
Vector Time (GMT): 2013/255/12:22:38
082
Vector Time (MET): N/A
Weight (LBS) : 957467
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5978979
29 A = 6798941
30 meter
Y = 2966414
00 meter E =
0012660
Z = -1270022
65 I = 51
87308
XDOT = -1149
377887 Wp = 42
65878
YDOT = 4805
419178 meter/sec RA = 34
97683 deg
ZDOT = 5856
284443 TA = 303
59469
MA = 303
71546
Ha = 227
812 n
mi
Hp = 219
070
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19616073
78 X = 5951533
26
Y = 9732329
39 feet Y = 3033121
22 meter
Z = -4166740
99 Z = -1241044
08
XDOT = -3770
924827 XDOT = -1231
476015
YDOT = 15765
810953 feet/sec YDOT = 4792
107371 meter/sec
ZDOT = 19213
531637 ZDOT = 5850
501196
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19013164
65 X = -5795212
59
Y = -10908856
50 feet Y = -3325019
46 meter
Z = -4045582
31 Z = -1233093
49
XDOT = 4046
658047 XDOT = 1233
421373
YDOT = -14114
962249 feet/sec YDOT = -4302
240494 meter/sec
ZDOT = 19188
537073 ZDOT = 5848
666100
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 13255
51811700
00016717 00000-0 10270-3 0 9107
2 25544 51
6483 35
5641 0003714 55
5029 304
6473 15
50606320 8254
Satellite: ISS
Catalog Number: 25544
Epoch time: 13255
51811700 = yrday
fracday
Element set: 910
Inclination: 51
6483 deg
RA of node: 35
5641 deg
Eccentricity:
0003714
Arg of perigee: 55
5029 deg
Mean anomaly: 304
6473 deg
Mean motion: 15
50606320 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 825
Checksum: 275
Coasting Arc #12 (Orbit 834)
---------------------------------------
Vector Time (GMT): 2013/256/03:27:52
994
Vector Time (MET): N/A
Weight (LBS) : 957320
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 963642
93 A = 6788819
62 meter
Y = -4241247
63 meter E =
0016533
Z = -5227179
53 I = 51
82254
XDOT = 6873
750343 Wp = 73
79832
YDOT = 3113
065340 meter/sec RA = 31
89475 deg
ZDOT = -1257
512594 TA = 184
12455
MA = 184
13819
Ha = 227
785 n
mi
Hp = 219
839
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3161558
18 X = 1036390
08
Y = -13914854
44 feet Y = -4230065
07 meter
Z = -17149539
13 Z = -5222321
33
XDOT = 22551
674355 XDOT = 6844
537143
YDOT = 10213
468963 feet/sec YDOT = 3189
768577 meter/sec
ZDOT = -4125
697488 ZDOT = -1224
191668
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7196679
50 X = -2193547
91
Y = -12351003
62 feet Y = -3764585
90 meter
Z = -17128509
28 Z = -5220769
63
XDOT = 22514
230614 XDOT = 6862
337491
YDOT = -7584
884777 feet/sec YDOT = -2311
872880 meter/sec
ZDOT = -3986
340473 ZDOT = -1215
036576
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 13256
16259574
00016717 00000-0 10270-3 0 9115
2 25544 51
6498 32
3732 0003003 42
1692 317
9690 15
50367555 8358
Satellite: ISS
Catalog Number: 25544
Epoch time: 13256
16259574 = yrday
fracday
Element set: 911
Inclination: 51
6498 deg
RA of node: 32
3732 deg
Eccentricity:
0003003
Arg of perigee: 42
1692 deg
Mean anomaly: 317
9690 deg
Mean motion: 15
50367555 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 835
Checksum: 307
Coasting Arc #13 (Orbit 850)
---------------------------------------
Vector Time (GMT): 2013/257/03:27:52
994
Vector Time (MET): N/A
Weight (LBS) : 957320
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1141523
50 A = 6788369
72 meter
Y = 4091370
14 meter E =
0004805
Z = 5291062
41 I = 51
79457
XDOT = -7046
904744 Wp = 80
67776
YDOT = -2926
438004 meter/sec RA = 26
94611 deg
ZDOT = 742
745082 TA = 2
24120
MA = 2
23904
Ha = 227
777 n
mi
Hp = 219
754
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3745155
85 X = -1212891
69
Y = 13423130
40 feet Y = 4078206
16 meter
Z = 17359128
65 Z = 5285343
44
XDOT = -23119
766222 XDOT = -7017
264968
YDOT = -9601
174554 feet/sec YDOT = -3005
075200 meter/sec
ZDOT = 2436
827698 ZDOT = 708
584176
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6646176
83 X = 2025754
70
Y = 12283695
12 feet Y = 3744070
27 meter
Z = 17334507
12 Z = 5283557
77
XDOT = -22345
823860 XDOT = -6811
007113
YDOT = 8854
082094 feet/sec YDOT = 2698
724222 meter/sec
ZDOT = 2293
919676 ZDOT = 699
186717
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 13257
19392783
00016717 00000-0 10270-3 0 9120
2 25544 51
6496 27
2611 0002929 43
8362 316
3020 15
50403733 8510
Satellite: ISS
Catalog Number: 25544
Epoch time: 13257
19392783 = yrday
fracday
Element set: 912
Inclination: 51
6496 deg
RA of node: 27
2611 deg
Eccentricity:
0002929
Arg of perigee: 43
8362 deg
Mean anomaly: 316
3020 deg
Mean motion: 15
50403733 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 851
Checksum: 294
Coasting Arc #14 (Orbit 865)
---------------------------------------
Vector Time (GMT): 2013/258/03:27:52
994
Vector Time (MET): N/A
Weight (LBS) : 957320
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1352949
20 A = 6788170
51 meter
Y = -3989148
83 meter E =
0017189
Z = -5337879
22 I = 51
76672
XDOT = 7150
799825 Wp = 81
32678
YDOT = 2709
516962 meter/sec RA = 21
99496 deg
ZDOT = -210
499130 TA = 186
65424
MA = 186
67710
Ha = 227
743 n
mi
Hp = 219
697
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4438809
70 X = 1423385
95
Y = -13087758
62 feet Y = -3973625
85 meter
Z = -17512727
09 Z = -5331135
38
XDOT = 23460
629346 XDOT = 7120
992488
YDOT = 8889
491346 feet/sec YDOT = 2789
315069 meter/sec
ZDOT = -690
613942 ZDOT = -175
834063
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6130056
38 X = -1868441
18
Y = -12426846
28 feet Y = -3787702
74 meter
Z = -17483820
17 Z = -5329068
39
XDOT = 21896
188040 XDOT = 6673
958115
YDOT = -10024
642036 feet/sec YDOT = -3055
510892 meter/sec
ZDOT = -545
559678 ZDOT = -166
286590
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 13258
16078504
00016717 00000-0 10270-3 0 9131
2 25544 51
6501 22
4684 0003049 45
7203 314
4198 15
50425248 8669
Satellite: ISS
Catalog Number: 25544
Epoch time: 13258
16078504 = yrday
fracday
Element set: 913
Inclination: 51
6501 deg
RA of node: 22
4684 deg
Eccentricity:
0003049
Arg of perigee: 45
7203 deg
Mean anomaly: 314
4198 deg
Mean motion: 15
50425248 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 866
Checksum: 294
Coasting Arc #15 (Orbit 881)
---------------------------------------
Vector Time (GMT): 2013/259/03:27:52
994
Vector Time (MET): N/A
Weight (LBS) : 957320
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1595233
06 A = 6788070
51 meter
Y = 3898649
48 meter E =
0005478
Z = 5319025
73 I = 51
73807
XDOT = -7240
226539 Wp = 58
78500
YDOT = -2497
797439 meter/sec RA = 17
04164 deg
ZDOT = -337
599613 TA = 34
44779
MA = 34
41229
Ha = 227
741 n
mi
Hp = 219
590
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5233704
28 X = -1664548
21
Y = 12790844
75 feet Y = 3880423
52 meter
Z = 17450871
81 Z = 5311107
56
XDOT = -23754
024077 XDOT = -7210
117557
YDOT = -8194
873488 feet/sec YDOT = -2578
593935 meter/sec
ZDOT = -1107
610278 ZDOT = -372
698288
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5579989
01 X = 1700780
65
Y = 12690165
73 feet Y = 3867962
52 meter
Z = 17417052
36 Z = 5308717
56
XDOT = -21385
176091 XDOT = -6518
201673
YDOT = 11138
733319 feet/sec YDOT = 3395
085916 meter/sec
ZDOT = -1254
512302 ZDOT = -382
375350
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 13259
19207873
00016717 00000-0 10270-3 0 9149
2 25544 51
6502 17
3560 0003002 47
4073 312
7331 15
50467507 8821
Satellite: ISS
Catalog Number: 25544
Epoch time: 13259
19207873 = yrday
fracday
Element set: 914
Inclination: 51
6502 deg
RA of node: 17
3560 deg
Eccentricity:
0003002
Arg of perigee: 47
4073 deg
Mean anomaly: 312
7331 deg
Mean motion: 15
50467507 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 882
Checksum: 284
Coasting Arc #16 (Orbit 896)
---------------------------------------
Vector Time (GMT): 2013/260/03:27:52
994
Vector Time (MET): N/A
Weight (LBS) : 957320
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1851599
13 A = 6788280
20 meter
Y = -3865312
03 meter E =
0016615
Z = -5278518
94 I = 51
70936
XDOT = 7252
423389 Wp = 88
79858
YDOT = 2268
155988 meter/sec RA = 12
08601 deg
ZDOT = 885
852770 TA = 189
66925
MA = 189
70127
Ha = 227
695 n
mi
Hp = 219
569
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6074800
31 X = 1920325
71
Y = -12681469
93 feet Y = -3844222
62 meter
Z = -17317975
54 Z = -5269356
73
XDOT = 23794
039989 XDOT = 7222
218153
YDOT = 7441
456655 feet/sec YDOT = 2349
088412 meter/sec
ZDOT = 2906
341110 ZDOT = 921
010479
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5148053
14 X = -1569126
60
Y = -13136620
75 feet Y = -4004042
00 meter
Z = -17278943
82 Z = -5266622
08
XDOT = 20615
878567 XDOT = 6283
719787
YDOT = -12083
527165 feet/sec YDOT = -3683
059080 meter/sec
ZDOT = 3053
519215 ZDOT = 930
712657
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 13260
15889986
00016717 00000-0 10270-3 0 9159
2 25544 51
6504 12
5630 0003078 49
1214 311
0203 15
50482018 8977
Satellite: ISS
Catalog Number: 25544
Epoch time: 13260
15889986 = yrday
fracday
Element set: 915
Inclination: 51
6504 deg
RA of node: 12
5630 deg
Eccentricity:
0003078
Arg of perigee: 49
1214 deg
Mean anomaly: 311
0203 deg
Mean motion: 15
50482018 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 897
Checksum: 290
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