[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
May 29th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 18298 65 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 128 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 423 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
There are no maneuvers
Coasting Arc #1 (Orbit 796)
---------------------------------------
Vector Time (GMT): 2014/146/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 884909
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5847896
24 A = 6799745
12 meter
Y = -3398192
78 meter E =
0016698
Z = 612174
92 I = 51
50298
XDOT = 2880
977220 Wp = 47
84157
YDOT = -3867
487361 meter/sec RA = 206
03255 deg
ZDOT = 5959
027858 TA = 318
77228
MA = 318
89827
Ha = 227
718 n
mi
Hp = 219
517
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19186011
29 X = -5812436
05
Y = -11148926
44 feet Y = -3463389
48 meter
Z = 2008447
90 Z = 583852
03
XDOT = 9452
024999 XDOT = 2895
062647
YDOT = -12688
606829 feet/sec YDOT = -3835
192092 meter/sec
ZDOT = 19550
616331 ZDOT = 5973
057435
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18616793
92 X = -5674398
79
Y = 12094699
02 feet Y = 3686464
26 meter
Z = 1889098
35 Z = 575797
18
XDOT = -6224
776853 XDOT = -1897
311985
YDOT = -12695
450092 feet/sec YDOT = -3869
573188 meter/sec
ZDOT = 19610
593593 ZDOT = 5977
308927
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 14146
56334488
00016717 00000-0 10270-3 0 9004
2 25544 51
6464 206
7921 0003793 34
5607 325
5790 15
50505921 7979
Satellite: ISS
Catalog Number: 25544
Epoch time: 14146
56334488 = yrday
fracday
Element set: 900
Inclination: 51
6464 deg
RA of node: 206
7921 deg
Eccentricity:
0003793
Arg of perigee: 34
5607 deg
Mean anomaly: 325
5790 deg
Mean motion: 15
50505921 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 797
Checksum: 317
Coasting Arc #2 (Orbit 811)
---------------------------------------
Vector Time (GMT): 2014/147/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 884909
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5860272
50 A = 6799123
64 meter
Y = 3243554
50 meter E =
0009319
Z = -1157809
51 I = 51
52989
XDOT = -3220
705374 Wp = 118
77324
YDOT = 3743
794449 meter/sec RA = 201
06916 deg
ZDOT = -5853
798495 TA = 73
79234
MA = 73
68982
Ha = 227
688 n
mi
Hp = 219
308
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19226615
81 X = 5829191
15
Y = 10641583
02 feet Y = 3308914
15 meter
Z = -3798587
62 Z = -1129415
83
XDOT = -10566
618680 XDOT = -3233
893593
YDOT = 12282
790187 feet/sec YDOT = 3707
705234 meter/sec
ZDOT = -19205
375640 ZDOT = -5869
476206
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17971917
42 X = 5477840
43
Y = -12681134
93 feet Y = -3865209
93 meter
Z = -3678901
13 Z = -1121329
06
XDOT = 5570
454732 XDOT = 1697
874602
YDOT = 13446
066961 feet/sec YDOT = 4098
361210 meter/sec
ZDOT = -19272
318114 ZDOT = -5874
202561
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 14147
53009672
00016717 00000-0 10270-3 0 9017
2 25544 51
6464 201
9986 0003793 39
1154 321
0270 15
50581455 8123
Satellite: ISS
Catalog Number: 25544
Epoch time: 14147
53009672 = yrday
fracday
Element set: 901
Inclination: 51
6464 deg
RA of node: 201
9986 deg
Eccentricity:
0003793
Arg of perigee: 39
1154 deg
Mean anomaly: 321
0270 deg
Mean motion: 15
50581455 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 812
Checksum: 294
Coasting Arc #3 (Orbit 827)
---------------------------------------
Vector Time (GMT): 2014/148/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 884909
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5833864
39 A = 6798616
11 meter
Y = -3053028
10 meter E =
0017680
Z = 1656114
81 I = 51
55632
XDOT = 3558
500757 Wp = 59
08093
YDOT = -3685
711539 meter/sec RA = 196
10703 deg
ZDOT = 5704
319289 TA = 319
06480
MA = 319
19741
Ha = 227
826 n
mi
Hp = 219
248
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19139975
02 X = -5807336
14
Y = -10016496
40 feet Y = -3118117
96 meter
Z = 5433447
53 Z = 1627838
39
XDOT = 11674
871249 XDOT = 3571
740566
YDOT = -12092
229460 feet/sec YDOT = -3645
844664 meter/sec
ZDOT = 18714
958296 ZDOT = 5721
638030
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17151763
98 X = -5227857
66
Y = 13182083
67 feet Y = 4017899
10 meter
Z = 5314212
89 Z = 1619772
09
XDOT = -5146
511815 XDOT = -1568
656801
YDOT = -14320
036976 feet/sec YDOT = -4364
747270 meter/sec
ZDOT = 18788
848739 ZDOT = 5726
841096
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 14148
56128473
00016717 00000-0 10270-3 0 9023
2 25544 51
6454 196
8857 0003996 42
4229 317
7230 15
50561485 8282
Satellite: ISS
Catalog Number: 25544
Epoch time: 14148
56128473 = yrday
fracday
Element set: 902
Inclination: 51
6454 deg
RA of node: 196
8857 deg
Eccentricity:
0003996
Arg of perigee: 42
4229 deg
Mean anomaly: 317
7230 deg
Mean motion: 15
50561485 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 828
Checksum: 329
Coasting Arc #4 (Orbit 842)
---------------------------------------
Vector Time (GMT): 2014/149/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 884909
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5745542
06 A = 6797550
01 meter
Y = 2900986
90 meter E =
0007301
Z = -2188528
90 I = 51
58413
XDOT = -3920
400329 Wp = 105
73721
YDOT = 3649
928977 meter/sec RA = 191
14605 deg
ZDOT = -5471
263247 TA = 98
52216
MA = 98
43941
Ha = 227
738 n
mi
Hp = 219
105
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18850203
60 X = 5723306
84
Y = 9517673
55 feet Y = 2965113
17 meter
Z = -7180212
94 Z = -2160671
19
XDOT = -12862
205804 XDOT = -3934
345319
YDOT = 11974
832601 feet/sec YDOT = 3606
011201 meter/sec
ZDOT = -17950
338736 ZDOT = -5490
341695
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16353338
05 X = 4984497
44
Y = -13422301
92 feet Y = -4091117
63 meter
Z = -7062711
19 Z = -2152714
37
XDOT = 4805
901993 XDOT = 1464
838927
YDOT = 15313
358608 feet/sec YDOT = 4667
511704 meter/sec
ZDOT = -18031
685434 ZDOT = -5496
057720
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 14149
52800511
00016717 00000-0 10270-3 0 9031
2 25544 51
6459 192
0917 0003945 46
1120 314
0357 15
50632521 8434
Satellite: ISS
Catalog Number: 25544
Epoch time: 14149
52800511 = yrday
fracday
Element set: 903
Inclination: 51
6459 deg
RA of node: 192
0917 deg
Eccentricity:
0003945
Arg of perigee: 46
1120 deg
Mean anomaly: 314
0357 deg
Mean motion: 15
50632521 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 843
Checksum: 279
Coasting Arc #5 (Orbit 858)
---------------------------------------
Vector Time (GMT): 2014/150/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 884909
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5614859
64 A = 6796630
47 meter
Y = -2730686
22 meter E =
0017349
Z = 2662797
11 I = 51
61029
XDOT = 4267
039821 Wp = 71
36306
YDOT = -3681
491305 meter/sec RA = 186
18620 deg
ZDOT = 5199
899242 TA = 318
66995
MA = 318
80111
Ha = 227
898 n
mi
Hp = 218
992
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18421455
52 X = -5596842
31
Y = -8958944
28 feet Y = -2793374
76 meter
Z = 8736210
99 Z = 2635564
09
XDOT = 13999
474479 XDOT = 4282
630284
YDOT = -12078
383546 feet/sec YDOT = -3633
687976 meter/sec
ZDOT = 17060
036882 ZDOT = 5220
665545
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15442174
36 X = -4706774
74
Y = 13533156
77 feet Y = 4124906
18 meter
Z = 8621311
24 Z = 2627775
67
XDOT = -4731
595491 XDOT = -1442
190306
YDOT = -16370
913802 feet/sec YDOT = -4989
854527 meter/sec
ZDOT = 17148
548155 ZDOT = 5226
877478
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 14150
55915957
00016717 00000-0 10270-3 0 9048
2 25544 51
6447 186
9783 0004145 49
9583 310
1931 15
50621385 8599
Satellite: ISS
Catalog Number: 25544
Epoch time: 14150
55915957 = yrday
fracday
Element set: 904
Inclination: 51
6447 deg
RA of node: 186
9783 deg
Eccentricity:
0004145
Arg of perigee: 49
9583 deg
Mean anomaly: 310
1931 deg
Mean motion: 15
50621385 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 859
Checksum: 331
Coasting Arc #6 (Orbit 873)
---------------------------------------
Vector Time (GMT): 2014/151/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 884909
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5424979
11 A = 6795258
59 meter
Y = 2614666
68 meter E =
0007706
Z = -3155860
96 I = 51
63830
XDOT = -4608
985669 Wp = 80
73220
YDOT = 3732
524800 meter/sec RA = 181
22729 deg
ZDOT = -4839
387617 TA = 135
56447
MA = 135
50262
Ha = 227
758 n
mi
Hp = 218
934
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17798487
88 X = 5410668
36
Y = 8578302
75 feet Y = 2675252
63 meter
Z = -10353874
55 Z = -3129541
46
XDOT = -15121
344060 XDOT = -4626
872725
YDOT = 12245
816273 feet/sec YDOT = 3680
884717 meter/sec
ZDOT = -15877
255962 ZDOT = -4861
820572
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14625099
58 X = 4457730
35
Y = -13370396
13 feet Y = -4075296
74 meter
Z = -10242809
02 Z = -3122008
19
XDOT = 4777
505925 XDOT = 1456
183806
YDOT = 17439
718235 feet/sec YDOT = 5315
626118 meter/sec
ZDOT = -15972
846686 ZDOT = -4868
523670
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 14151
52584901
00016717 00000-0 10270-3 0 9058
2 25544 51
6457 182
1842 0004042 52
9676 307
1844 15
50680127 8742
Satellite: ISS
Catalog Number: 25544
Epoch time: 14151
52584901 = yrday
fracday
Element set: 905
Inclination: 51
6457 deg
RA of node: 182
1842 deg
Eccentricity:
0004042
Arg of perigee: 52
9676 deg
Mean anomaly: 307
1844 deg
Mean motion: 15
50680127 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 874
Checksum: 304
Coasting Arc #7 (Orbit 889)
---------------------------------------
Vector Time (GMT): 2014/152/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 884909
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5194949
97 A = 6794048
82 meter
Y = -2498619
53 meter E =
0015703
Z = 3580499
67 I = 51
66407
XDOT = 4924
502620 Wp = 83
82978
YDOT = -3844
909356 meter/sec RA = 176
26917 deg
ZDOT = 4446
707009 TA = 318
44290
MA = 318
56216
Ha = 227
919 n
mi
Hp = 218
781
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17043799
13 X = -5184016
72
Y = -8197570
65 feet Y = -2556652
06 meter
Z = 11747046
16 Z = 3555289
52
XDOT = 16156
504659 XDOT = 4945
530516
YDOT = -12614
532009 feet/sec YDOT = -3789
723316 meter/sec
ZDOT = 14588
933758 ZDOT = 4470
680300
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13770741
09 X = -4197321
88
Y = 13059341
49 feet Y = 3980487
29 meter
Z = 11640645
88 Z = 3548068
86
XDOT = -5089
469786 XDOT = -1551
270391
YDOT = -18506
465391 feet/sec YDOT = -5640
770651 meter/sec
ZDOT = 14691
079700 ZDOT = 4477
841093
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 14152
55697009
00016717 00000-0 10270-3 0 9067
2 25544 51
6444 177
0703 0004207 56
7359 303
4195 15
50681138 8909
Satellite: ISS
Catalog Number: 25544
Epoch time: 14152
55697009 = yrday
fracday
Element set: 906
Inclination: 51
6444 deg
RA of node: 177
0703 deg
Eccentricity:
0004207
Arg of perigee: 56
7359 deg
Mean anomaly: 303
4195 deg
Mean motion: 15
50681138 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 890
Checksum: 310
Coasting Arc #8 (Orbit 904)
---------------------------------------
Vector Time (GMT): 2014/153/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 884909
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4916518
48 A = 6792579
31 meter
Y = 2450810
23 meter E =
0010795
Z = -4006787
16 I = 51
69145
XDOT = -5205
804803 Wp = 68
34196
YDOT = 3965
642615 meter/sec RA = 171
31208 deg
ZDOT = -3966
849287 TA = 160
33298
MA = 160
29131
Ha = 227
754 n
mi
Hp = 218
787
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16130309
98 X = 4908211
28
Y = 8040715
97 feet Y = 2505743
84 meter
Z = -13145627
17 Z = -3982923
29
XDOT = -17079
412082 XDOT = -5230
492889
YDOT = 13010
638500 feet/sec YDOT = 3907
290310 meter/sec
ZDOT = -13014
597397 ZDOT = -3992
197995
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13087884
90 X = 3989187
32
Y = -12497405
90 feet Y = -3809209
32 meter
Z = -13044908
65 Z = -3976088
16
XDOT = 5519
445989 XDOT = 1682
327137
YDOT = 19461
425731 feet/sec YDOT = 5931
842563 meter/sec
ZDOT = -13122
602106 ZDOT = -3999
769122
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 14153
52362891
00016717 00000-0 10270-3 0 9074
2 25544 51
6453 172
2762 0004095 59
5717 300
5838 15
50725001 9052
Satellite: ISS
Catalog Number: 25544
Epoch time: 14153
52362891 = yrday
fracday
Element set: 907
Inclination: 51
6453 deg
RA of node: 172
2762 deg
Eccentricity:
0004095
Arg of perigee: 59
5717 deg
Mean anomaly: 300
5838 deg
Mean motion: 15
50725001 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 905
Checksum: 300
Coasting Arc #9 (Orbit 920)
---------------------------------------
Vector Time (GMT): 2014/154/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 884909
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4605352
98 A = 6791288
00 meter
Y = -2419335
03 meter E =
0012985
Z = 4355194
06 I = 51
71679
XDOT = 5453
711503 Wp = 95
12506
YDOT = -4134
341650 meter/sec RA = 166
35539 deg
ZDOT = 3460
303147 TA = 319
73874
MA = 319
83483
Ha = 227
890 n
mi
Hp = 218
622
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15109425
77 X = -4599113
31
Y = -7937450
88 feet Y = -2470800
53 meter
Z = 14288694
44 Z = 4332836
81
XDOT = 17892
754274 XDOT = 5482
728244
YDOT = -13564
113026 feet/sec YDOT = -4073
192799 meter/sec
ZDOT = 11352
700613 ZDOT = 3486
866691
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12443860
47 X = -3792888
67
Y = 11795577
40 feet Y = 3595291
99 meter
Z = 14194342
28 Z = 4326435
53
XDOT = -6176
791771 XDOT = -1882
686132
YDOT = -20353
681040 feet/sec YDOT = -6203
801981 meter/sec
ZDOT = 11465
891854 ZDOT = 3494
803837
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 14154
55471658
00016717 00000-0 10270-3 0 9081
2 25544 51
6442 167
1620 0004187 62
7812 297
3765 15
50736790 9217
Satellite: ISS
Catalog Number: 25544
Epoch time: 14154
55471658 = yrday
fracday
Element set: 908
Inclination: 51
6442 deg
RA of node: 167
1620 deg
Eccentricity:
0004187
Arg of perigee: 62
7812 deg
Mean anomaly: 297
3765 deg
Mean motion: 15
50736790 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 921
Checksum: 322
Coasting Arc #10 (Orbit 935)
---------------------------------------
Vector Time (GMT): 2014/155/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 884909
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4264389
08 A = 6789970
35 meter
Y = 2465045
45 meter E =
0014560
Z = -4687776
35 I = 51
74302
XDOT = -5641
817646 Wp = 69
48708
YDOT = 4292
593272 meter/sec RA = 161
39979 deg
ZDOT = -2877
301240 TA = 171
90906
MA = 171
88555
Ha = 227
732 n
mi
Hp = 218
654
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13990777
83 X = 4259279
22
Y = 8087419
45 feet Y = 2512704
37 meter
Z = -15379843
65 Z = -4667072
71
XDOT = -18509
900413 XDOT = -5675
422044
YDOT = 14083
311259 feet/sec YDOT = 4229
315165 meter/sec
ZDOT = -9439
964698 ZDOT = -2904
789775
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12038589
28 X = 3669362
01
Y = -10904116
33 feet Y = -3323574
66 meter
Z = -15292495
67 Z = -4661152
68
XDOT = 6906
348486 XDOT = 2105
055019
YDOT = 21017
740256 feet/sec YDOT = 6406
207230 meter/sec
ZDOT = -9557
113322 ZDOT = -2913
008141
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 14155
52134461
00016717 00000-0 10270-3 0 9098
2 25544 51
6445 162
3679 0004120 65
9388 294
2194 15
50767711 9366
Satellite: ISS
Catalog Number: 25544
Epoch time: 14155
52134461 = yrday
fracday
Element set: 909
Inclination: 51
6445 deg
RA of node: 162
3679 deg
Eccentricity:
0004120
Arg of perigee: 65
9388 deg
Mean anomaly: 294
2194 deg
Mean motion: 15
50767711 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 936
Checksum: 318
Coasting Arc #11 (Orbit 951)
---------------------------------------
Vector Time (GMT): 2014/156/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 884909
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3901914
36 A = 6788854
41 meter
Y = -2539197
56 meter E =
0009723
Z = 4933756
52 I = 51
76787
XDOT = 5795
081235 Wp = 102
00272
YDOT = -4479
191032 meter/sec RA = 156
44450 deg
ZDOT = 2272
093779 TA = 325
80658
MA = 325
86916
Ha = 227
829 n
mi
Hp = 218
501
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12801556
30 X = -3897197
18
Y = -8330700
64 feet Y = -2582805
22 meter
Z = 16186865
24 Z = 4914812
78
XDOT = 19012
733712 XDOT = 5833
700713
YDOT = -14695
508634 feet/sec YDOT = -4414
170927 meter/sec
ZDOT = 7454
375914 ZDOT = 2300
339102
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11735851
22 X = -3577087
45
Y = 9906060
82 feet Y = 3019367
34 meter
Z = 16106979
18 Z = 4909407
25
XDOT = -7789
713154 XDOT = -2374
304569
YDOT = -21575
818042 feet/sec YDOT = -6576
309339 meter/sec
ZDOT = 7574
774289 ZDOT = 2308
791203
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 14156
55239848
00016717 00000-0 10270-3 0 9109
2 25544 51
6437 157
2535 0004130 68
4874 291
6716 15
50788095 9527
Satellite: ISS
Catalog Number: 25544
Epoch time: 14156
55239848 = yrday
fracday
Element set: 910
Inclination: 51
6437 deg
RA of node: 157
2535 deg
Eccentricity:
0004130
Arg of perigee: 68
4874 deg
Mean anomaly: 291
6716 deg
Mean motion: 15
50788095 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 952
Checksum: 330
Coasting Arc #12 (Orbit 966)
---------------------------------------
Vector Time (GMT): 2014/157/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 884909
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3534189
93 A = 6787935
55 meter
Y = 2691630
74 meter E =
0017546
Z = -5148049
21 I = 51
79302
XDOT = -5871
485999 Wp = 76
65457
YDOT = 4631
402057 meter/sec RA = 151
49025 deg
ZDOT = -1610
010161 TA = 177
81303
MA = 177
80535
Ha = 227
694 n
mi
Hp = 218
528
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11595111
32 X = 3528836
57
Y = 8830809
51 feet Y = 2731122
71 meter
Z = -16889925
22 Z = -5130893
33
XDOT = -19263
405510 XDOT = -5915
018041
YDOT = 15194
888640 feet/sec YDOT = 4565
500025 meter/sec
ZDOT = -5282
185567 ZDOT = -1638
638665
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11712999
20 X = 3570122
16
Y = -8813182
46 feet Y = -2686258
01 meter
Z = -16817634
84 Z = -5126015
10
XDOT = 8661
347654 XDOT = 2639
978765
YDOT = 21819
523304 feet/sec YDOT = 6650
590703 meter/sec
ZDOT = -5404
246067 ZDOT = -1647
214201
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 14157
51899499
00016717 00000-0 10270-3 0 9111
2 25544 51
6436 152
4591 0004125 72
0509 288
1091 15
50810876 9671
Satellite: ISS
Catalog Number: 25544
Epoch time: 14157
51899499 = yrday
fracday
Element set: 911
Inclination: 51
6436 deg
RA of node: 152
4591 deg
Eccentricity:
0004125
Arg of perigee: 72
0509 deg
Mean anomaly: 288
1091 deg
Mean motion: 15
50810876 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 967
Checksum: 326
Coasting Arc #13 (Orbit 982)
---------------------------------------
Vector Time (GMT): 2014/158/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 884909
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3158052
91 A = 6787248
88 meter
Y = -2878309
03 meter E =
0006976
Z = 5267527
35 I = 51
81731
XDOT = 5917
657006 Wp = 96
53014
YDOT = -4787
875630 meter/sec RA = 146
53662 deg
ZDOT = 929
781740 TA = 344
58605
MA = 344
60728
Ha = 227
748 n
mi
Hp = 218
396
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10361065
98 X = -3151220
49
Y = -9443271
11 feet Y = -2913586
54 meter
Z = 17281913
87 Z = 5252202
24
XDOT = 19414
885190 XDOT = 5966
239679
YDOT = -15708
253379 feet/sec YDOT = -4721
429003 meter/sec
ZDOT = 3050
465026 ZDOT = 958
646874
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11832057
21 X = -3606411
04
Y = 7665170
80 feet Y = 2336344
06 meter
Z = 17217409
31 Z = 5247866
36
XDOT = -9586
844628 XDOT = -2922
070243
YDOT = -21940
341199 feet/sec YDOT = -6687
415997 meter/sec
ZDOT = 3173
568709 ZDOT = 967
303743
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 14158
55001434
00016717 00000-0 10270-3 0 9121
2 25544 51
6429 147
3445 0004076 74
3211 285
8390 15
50838382 9830
Satellite: ISS
Catalog Number: 25544
Epoch time: 14158
55001434 = yrday
fracday
Element set: 912
Inclination: 51
6429 deg
RA of node: 147
3445 deg
Eccentricity:
0004076
Arg of perigee: 74
3211 deg
Mean anomaly: 285
8390 deg
Mean motion: 15
50838382 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 983
Checksum: 305
Coasting Arc #14 (Orbit 997)
---------------------------------------
Vector Time (GMT): 2014/159/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 884909
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2803843
86 A = 6786922
98 meter
Y = 3134675
81 meter E =
0018867
Z = -5343078
73 I = 51
84170
XDOT = -5881
857281 Wp = 86
17420
YDOT = 4885
176127 meter/sec RA = 141
58407 deg
ZDOT = -219
986256 TA = 181
72645
MA = 181
73297
Ha = 227
633 n
mi
Hp = 218
412
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9198962
81 X = 2794538
10
Y = 10284369
46 feet Y = 3165978
55 meter
Z = -17529785
86 Z = -5329480
26
XDOT = -19297
432025 XDOT = -5934
978641
YDOT = 16027
480733 feet/sec YDOT = 4819
104416 meter/sec
ZDOT = -721
739685 ZDOT = -248
688532
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12233044
76 X = 3728632
04
Y = -6537739
97 feet Y = -1992703
14 meter
Z = -17472639
65 Z = -5325660
56
XDOT = 10394
637307 XDOT = 3168
285451
YDOT = 21710
882311 feet/sec YDOT = 6617
476928 meter/sec
ZDOT = -844
185880 ZDOT = -257
307856
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 14159
51657824
00016717 00000-0 10270-3 0 9139
2 25544 51
6428 142
5496 0004105 77
9635 282
1975 15
50857740 9988
Satellite: ISS
Catalog Number: 25544
Epoch time: 14159
51657824 = yrday
fracday
Element set: 913
Inclination: 51
6428 deg
RA of node: 142
5496 deg
Eccentricity:
0004105
Arg of perigee: 77
9635 deg
Mean anomaly: 282
1975 deg
Mean motion: 15
50857740 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 998
Checksum: 341
Coasting Arc #15 (Orbit 1013)
---------------------------------------
Vector Time (GMT): 2014/160/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 884909
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2453868
49 A = 6786853
64 meter
Y = -3423303
14 meter E =
0006718
Z = 5316216
10 I = 51
86540
XDOT = 5826
418741 Wp = 76
52561
YDOT = -4960
474621 meter/sec RA = 136
63275 deg
ZDOT = -502
800699 TA = 18
26809
MA = 18
24397
Ha = 227
648 n
mi
Hp = 218
299
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8050749
63 X = -2441230
79
Y = -11231309
52 feet Y = -3450673
68 meter
Z = 17441653
86 Z = 5304325
77
XDOT = 19115
547050 XDOT = 5883
897340
YDOT = -16274
523034 feet/sec YDOT = -4894
998437 meter/sec
ZDOT = -1649
608593 ZDOT = -474
357189
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12781959
27 X = -3895941
19
Y = 5414345
19 feet Y = 1650292
41 meter
Z = 17391795
65 Z = 5301019
31
XDOT = -11142
317492 XDOT = -3396
178372
YDOT = -21373
628550 feet/sec YDOT = -6514
681982 meter/sec
ZDOT = -1528
227783 ZDOT = -465
803828
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 14160
54756218
00016717 00000-0 10270-3 0 9142
2 25544 51
6425 137
4348 0004030 80
5212 279
6394 15
50892218 10147
Satellite: ISS
Catalog Number: 25544
Epoch time: 14160
54756218 = yrday
fracday
Element set: 914
Inclination: 51
6425 deg
RA of node: 137
4348 deg
Eccentricity:
0004030
Arg of perigee: 80
5212 deg
Mean anomaly: 279
6394 deg
Mean motion: 15
50892218 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1014
Checksum: 293
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