[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
November 2nd 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15069 47 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 134 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 284 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 3950)
---------------------------------------
Vector Time (GMT): 2012/307/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6359322
16 A = 6796779
52 meter
Y = 1698845
67 meter E =
0002612
Z = 1700925
41 I = 51
81488
XDOT = 162
342553 Wp = 204
83210
YDOT = -5103
266197 meter/sec RA = 153
31674 deg
ZDOT = 5704
856793 TA = 173
72807
MA = 173
72480
Ha = 226
899 n
mi
Hp = 219
758
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20863917
86 X = -6386109
27
Y = 5573640
65 feet Y = 1627581
98 meter
Z = 5580463
93 Z = 1669966
34
XDOT = 532
619925 XDOT = 191
682736
YDOT = -16742
999335 feet/sec YDOT = -5101
286756 meter/sec
ZDOT = 18716
721762 ZDOT = 5705
716710
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12003305
26 X = 3658607
44
Y = -17991818
52 feet Y = -5483906
29 meter
Z = 5452086
33 Z = 1661795
91
XDOT = 9436
197294 XDOT = 2876
152935
YDOT = 11967
483455 feet/sec YDOT = 3647
688957 meter/sec
ZDOT = 18720
764570 ZDOT = 5706
089041
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 12307
56117115
00016717 00000-0 10270-3 0 9007
2 25544 51
6452 154
0523 0016009 238
1020 121
8574 15
51167618 39514
Satellite: ISS
Catalog Number: 25544
Epoch time: 12307
56117115 = yrday
fracday
Element set: 900
Inclination: 51
6452 deg
RA of node: 154
0523 deg
Eccentricity:
0016009
Arg of perigee: 238
1020 deg
Mean anomaly: 121
8574 deg
Mean motion: 15
51167618 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3951
Checksum: 275
Coasting Arc #2 (Orbit 3965)
---------------------------------------
Vector Time (GMT): 2012/308/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6153270
69 A = 6795681
99 meter
Y = -1603768
38 meter E =
0015298
Z = -2368526
75 I = 51
83717
XDOT = -674
890011 Wp = 221
08940
YDOT = 5402
222844 meter/sec RA = 148
37073 deg
ZDOT = -5402
715223 TA = 345
26608
MA = 345
31061
Ha = 226
706 n
mi
Hp = 219
814
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20187895
97 X = 6182253
03
Y = -5261707
29 feet Y = -1534796
60 meter
Z = -7770757
07 Z = -2338563
46
XDOT = -2214
206073 XDOT = -709
002937
YDOT = 17723
828229 feet/sec YDOT = 5394
485108 meter/sec
ZDOT = -17725
443644 ZDOT = -5406
076694
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11412306
85 X = -3478471
13
Y = 17518896
37 feet Y = 5339759
61 meter
Z = -7646495
61 Z = -2330651
86
XDOT = -9103
289188 XDOT = -2774
682544
YDOT = -13685
514084 feet/sec YDOT = -4171
344693 meter/sec
ZDOT = -17739
882273 ZDOT = -5407
116117
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 12308
52755170
00016717 00000-0 10270-3 0 9014
2 25544 51
6445 149
2568 0015956 241
9038 118
0500 15
51158528 39665
Satellite: ISS
Catalog Number: 25544
Epoch time: 12308
52755170 = yrday
fracday
Element set: 901
Inclination: 51
6445 deg
RA of node: 149
2568 deg
Eccentricity:
0015956
Arg of perigee: 241
9038 deg
Mean anomaly: 118
0500 deg
Mean motion: 15
51158528 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3966
Checksum: 313
Coasting Arc #3 (Orbit 3981)
---------------------------------------
Vector Time (GMT): 2012/309/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5918784
85 A = 6794053
72 meter
Y = 1444034
78 meter E =
0005196
Z = 3014613
69 I = 51
85746
XDOT = 1140
914109 Wp = 197
72297
YDOT = -5708
634011 meter/sec RA = 143
42302 deg
ZDOT = 4971
967332 TA = 196
60284
MA = 196
61986
Ha = 226
276 n
mi
Hp = 219
831
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19418585
46 X = -5949137
01
Y = 4737646
93 feet Y = 1377677
51 meter
Z = 9890464
86 Z = 2985786
28
XDOT = 3743
156527 XDOT = 1180
511335
YDOT = -18729
114208 feet/sec YDOT = -5695
654221 meter/sec
ZDOT = 16312
228778 ZDOT = 4977
606092
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10918594
90 X = 3327987
72
Y = -16812545
76 feet Y = -5124463
95 meter
Z = 9770908
12 Z = 2978172
80
XDOT = 8974
331307 XDOT = 2735
376182
YDOT = 15327
196624 feet/sec YDOT = 4671
729531 meter/sec
ZDOT = 16336
137320 ZDOT = 4979
254655
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 12309
55833622
00016717 00000-0 10270-3 0 9028
2 25544 51
6443 144
1394 0016048 245
7396 114
2079 15
51220212 39823
Satellite: ISS
Catalog Number: 25544
Epoch time: 12309
55833622 = yrday
fracday
Element set: 902
Inclination: 51
6443 deg
RA of node: 144
1394 deg
Eccentricity:
0016048
Arg of perigee: 245
7396 deg
Mean anomaly: 114
2079 deg
Mean motion: 15
51220212 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3982
Checksum: 295
Coasting Arc #4 (Orbit 3996)
---------------------------------------
Vector Time (GMT): 2012/310/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5625472
89 A = 6792388
23 meter
Y = -1212228
86 meter E =
0010847
Z = -3595457
34 I = 51
87533
XDOT = -1549
746454 Wp = 242
73694
YDOT = 6044
396469 meter/sec RA = 138
47653 deg
ZDOT = -4457
180004 TA = 339
60609
MA = 339
64937
Ha = 226
047 n
mi
Hp = 219
817
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18456275
87 X = 5656076
37
Y = -3977128
79 feet Y = -1149150
20 meter
Z = -11796119
88 Z = -3568054
28
XDOT = -5084
469995 XDOT = -1595
568668
YDOT = 19830
697077 feet/sec YDOT = 6026
810016 meter/sec
ZDOT = -14623
293976 ZDOT = -4464
820040
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10478776
81 X = -3193931
17
Y = 15789717
85 feet Y = 4812706
00 meter
Z = -11682472
50 Z = -3560817
62
XDOT = -9127
222004 XDOT = -2781
977267
YDOT = -16913
948893 feet/sec YDOT = -5155
371623 meter/sec
ZDOT = -14655
533755 ZDOT = -4467
006689
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 12310
52468075
00016717 00000-0 10270-3 0 9034
2 25544 51
6437 139
3434 0015837 249
4501 110
4951 15
51235241 39972
Satellite: ISS
Catalog Number: 25544
Epoch time: 12310
52468075 = yrday
fracday
Element set: 903
Inclination: 51
6437 deg
RA of node: 139
3434 deg
Eccentricity:
0015837
Arg of perigee: 249
4501 deg
Mean anomaly: 110
4951 deg
Mean motion: 15
51235241 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3997
Checksum: 300
Coasting Arc #5 (Orbit 4012)
---------------------------------------
Vector Time (GMT): 2012/311/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5323614
37 A = 6790604
34 meter
Y = 904786
06 meter E =
0008586
Z = 4126664
47 I = 51
89174
XDOT = 1891
265793 Wp = 215
64369
YDOT = -6352
675326 meter/sec RA = 133
52812 deg
ZDOT = 3829
900759 TA = 194
86186
MA = 194
88711
Ha = 225
667 n
mi
Hp = 219
843
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17465926
43 X = -5353382
91
Y = 2968458
22 feet Y = 845087
70 meter
Z = 13538925
41 Z = 4100729
89
XDOT = 6204
940266 XDOT = 1943
557109
YDOT = -20842
110649 feet/sec YDOT = -6331
233576 meter/sec
ZDOT = 12565
291205 ZDOT = 3839
215687
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10233386
30 X = 3119136
14
Y = -14561890
30 feet Y = -4438464
16 meter
Z = 13431380
68 Z = 4093884
83
XDOT = 9441
299601 XDOT = 2877
708118
YDOT = 18269
320969 feet/sec YDOT = 5568
489031 meter/sec
ZDOT = 12604
508911 ZDOT = 3841
854316
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 12311
55542760
00016717 00000-0 10270-3 0 9043
2 25544 51
6437 134
2262 0015980 253
2839 106
6558 15
51263365 40139
Satellite: ISS
Catalog Number: 25544
Epoch time: 12311
55542760 = yrday
fracday
Element set: 904
Inclination: 51
6437 deg
RA of node: 134
2262 deg
Eccentricity:
0015980
Arg of perigee: 253
2839 deg
Mean anomaly: 106
6558 deg
Mean motion: 15
51263365 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4013
Checksum: 296
Coasting Arc #6 (Orbit 4027)
---------------------------------------
Vector Time (GMT): 2012/312/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4992976
36 A = 6788861
25 meter
Y = -520641
71 meter E =
0006142
Z = -4564900
90 I = 51
90639
XDOT = -2170
147854 Wp = 267
89333
YDOT = 6654
004493 meter/sec RA = 128
58013 deg
ZDOT = -3129
157898 TA = 330
84998
MA = 330
88425
Ha = 225
451 n
mi
Hp = 219
750
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16381156
04 X = 5020602
78
Y = -1708142
08 feet Y = -464652
79 meter
Z = -14976708
99 Z = -4540577
76
XDOT = -7119
907656 XDOT = -2229
192061
YDOT = 21830
723401 feet/sec YDOT = 6629
406319 meter/sec
ZDOT = -10266
266070 ZDOT = -3139
844145
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10148682
72 X = -3093318
49
Y = 13087190
85 feet Y = 3988975
77 meter
Z = -14875870
05 Z = -4534165
19
XDOT = -9946
983413 XDOT = -3031
840544
YDOT = -19446
826933 feet/sec YDOT = -5927
392849 meter/sec
ZDOT = -10311
204649 ZDOT = -3142
855177
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 12312
52173533
00016717 00000-0 10270-3 0 9050
2 25544 51
6435 129
4299 0015714 256
6803 103
2596 15
51300987 40289
Satellite: ISS
Catalog Number: 25544
Epoch time: 12312
52173533 = yrday
fracday
Element set: 905
Inclination: 51
6435 deg
RA of node: 129
4299 deg
Eccentricity:
0015714
Arg of perigee: 256
6803 deg
Mean anomaly: 103
2596 deg
Mean motion: 15
51300987 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4028
Checksum: 303
Coasting Arc #7 (Orbit 4043)
---------------------------------------
Vector Time (GMT): 2012/313/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4678646
97 A = 6787447
84 meter
Y = 62490
43 meter E =
0011513
Z = 4927542
21 I = 51
91952
XDOT = 2377
332219 Wp = 238
24885
YDOT = -6888
582619 meter/sec RA = 123
63005 deg
ZDOT = 2342
736940 TA = 188
85997
MA = 188
88031
Ha = 225
137 n
mi
Hp = 219
822
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15349891
62 X = -4702935
31
Y = 205021
09 feet Y = 10035
27 meter
Z = 16166477
06 Z = 4904754
17
XDOT = 7799
646387 XDOT = 2442
804420
YDOT = -22600
336675 feet/sec YDOT = -6861
631632 meter/sec
ZDOT = 7686
144815 ZDOT = 2354
445424
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10331330
54 X = 3148989
55
Y = -11487792
87 feet Y = -3501479
27 meter
Z = 16072038
17 Z = 4898757
23
XDOT = 10502
731114 XDOT = 3201
232443
YDOT = 20276
258780 feet/sec YDOT = 6180
203676 meter/sec
ZDOT = 7735
352825 ZDOT = 2357
735541
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 12313
55244377
00016717 00000-0 10270-3 0 9060
2 25544 51
6432 124
3125 0015809 260
7443 99
1920 15
51300177 40442
Satellite: ISS
Catalog Number: 25544
Epoch time: 12313
55244377 = yrday
fracday
Element set: 906
Inclination: 51
6432 deg
RA of node: 124
3125 deg
Eccentricity:
0015809
Arg of perigee: 260
7443 deg
Mean anomaly: 99
1920 deg
Mean motion: 15
51300177 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4044
Checksum: 286
Coasting Arc #8 (Orbit 4058)
---------------------------------------
Vector Time (GMT): 2012/314/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4366020
52 A = 6786173
93 meter
Y = 460854
24 meter E =
0002386
Z = -5173109
33 I = 51
93235
XDOT = -2530
045443 Wp = 296
61595
YDOT = 7077
965872 meter/sec RA = 118
68068 deg
ZDOT = -1503
191063 TA = 318
95167
MA = 318
96962
Ha = 224
982 n
mi
Hp = 219
643
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14324214
30 X = 4385672
96
Y = 1511988
97 feet Y = 509787
44 meter
Z = -16972143
46 Z = -5151851
25
XDOT = -8300
674026 XDOT = -2601
702387
YDOT = 23221
672810 feet/sec YDOT = 7049
272593 meter/sec
ZDOT = -4931
729209 ZDOT = -1515
656559
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10733640
48 X = -3271613
62
Y = 9759059
46 feet Y = 2974561
32 meter
Z = -16884093
10 Z = -5146271
58
XDOT = -11107
751223 XDOT = -3385
642573
YDOT = -20848
977353 feet/sec YDOT = -6354
768297 meter/sec
ZDOT = -4984
105226 ZDOT = -1519
155273
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 12314
51871342
00016717 00000-0 10270-3 0 9076
2 25544 51
6436 119
5161 0015613 263
9460 95
9912 15
51362859 40595
Satellite: ISS
Catalog Number: 25544
Epoch time: 12314
51871342 = yrday
fracday
Element set: 907
Inclination: 51
6436 deg
RA of node: 119
5161 deg
Eccentricity:
0015613
Arg of perigee: 263
9460 deg
Mean anomaly: 95
9912 deg
Mean motion: 15
51362859 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4059
Checksum: 315
Coasting Arc #9 (Orbit 4074)
---------------------------------------
Vector Time (GMT): 2012/315/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4093160
05 A = 6785623
85 meter
Y = -1042277
21 meter E =
0013051
Z = 5322084
41 I = 51
94340
XDOT = 2623
798940 Wp = 262
20906
YDOT = -7164
287992 meter/sec RA = 113
72923 deg
ZDOT = 614
450561 TA = 181
93700
MA = 181
94206
Ha = 224
791 n
mi
Hp = 219
792
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13429002
80 X = -4107054
99
Y = -3419544
66 feet Y = -1088126
93 meter
Z = 17460906
86 Z = 5302165
84
XDOT = 8608
264240 XDOT = 2700
731564
YDOT = -23504
881863 feet/sec YDOT = -7134
516849 meter/sec
ZDOT = 2015
913913 ZDOT = 627
384374
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11426556
76 X = 3482814
50
Y = -8021061
71 feet Y = -2444819
61 meter
Z = 17378464
83 Z = 5296956
08
XDOT = 11607
012914 XDOT = 3537
817536
YDOT = 21023
495345 feet/sec YDOT = 6407
961381 meter/sec
ZDOT = 2070
253946 ZDOT = 631
013403
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 12315
54938249
00016717 00000-0 10270-3 0 9081
2 25544 51
6430 114
3981 0015610 268
1174 91
8189 15
51338907 40754
Satellite: ISS
Catalog Number: 25544
Epoch time: 12315
54938249 = yrday
fracday
Element set: 908
Inclination: 51
6430 deg
RA of node: 114
3981 deg
Eccentricity:
0015610
Arg of perigee: 268
1174 deg
Mean anomaly: 91
8189 deg
Mean motion: 15
51338907 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4075
Checksum: 319
Coasting Arc #10 (Orbit 4089)
---------------------------------------
Vector Time (GMT): 2012/316/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3846121
07 A = 6785258
85 meter
Y = 1661299
87 meter E =
0000773
Z = -5336701
48 I = 51
95535
XDOT = -2685
128379 Wp = 255
36719
YDOT = 7173
232049 meter/sec RA = 108
77966 deg
ZDOT = 297
628481 TA = 17
46024
MA = 17
45758
Ha = 224
766 n
mi
Hp = 219
549
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12618507
44 X = 3853183
43
Y = 5450458
88 feet Y = 1704348
91 meter
Z = -17508863
11 Z = -5317999
57
XDOT = -8809
476308 XDOT = -2766
587246
YDOT = 23534
225881 feet/sec YDOT = 7142
749812 meter/sec
ZDOT = 976
471394 ZDOT = 284
385781
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12329485
75 X = -3758027
26
Y = 6294453
83 feet Y = 1918549
53 meter
Z = -17431527
52 Z = -5313129
59
XDOT = -11989
326380 XDOT = -3654
346681
YDOT = -20932
351711 feet/sec YDOT = -6380
180802 meter/sec
ZDOT = 920
832856 ZDOT = 280
669854
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 12316
51561314
00016717 00000-0 10270-3 0 9095
2 25544 51
6439 109
6017 0015561 271
4024 88
5345 15
51423317 40900
Satellite: ISS
Catalog Number: 25544
Epoch time: 12316
51561314 = yrday
fracday
Element set: 909
Inclination: 51
6439 deg
RA of node: 109
6017 deg
Eccentricity:
0015561
Arg of perigee: 271
4024 deg
Mean anomaly: 88
5345 deg
Mean motion: 15
51423317 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4090
Checksum: 289
Coasting Arc #11 (Orbit 4105)
---------------------------------------
Vector Time (GMT): 2012/317/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3654292
98 A = 6785806
40 meter
Y = -2309444
37 meter E =
0012648
Z = 5241737
38 I = 51
96550
XDOT = 2714
369739 Wp = 287
04390
YDOT = -7053
417280 meter/sec RA = 103
82889 deg
ZDOT = -1214
130286 TA = 174
58062
MA = 174
56692
Ha = 224
729 n
mi
Hp = 219
745
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11989150
20 X = -3653660
65
Y = -7576917
23 feet Y = -2350305
39 meter
Z = 17197301
13 Z = 5223986
00
XDOT = 8905
412528 XDOT = 2798
938938
YDOT = -23141
132807 feet/sec YDOT = -7022
590656 meter/sec
ZDOT = -3983
367079 ZDOT = -1200
738125
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13481468
84 X = 4109151
70
Y = -4681455
69 feet Y = -1426907
69 meter
Z = 17123975
41 Z = 5219387
71
XDOT = 12102
743993 XDOT = 3688
916369
YDOT = 20474
020318 feet/sec YDOT = 6240
481393 meter/sec
ZDOT = -3927
101574 ZDOT = -1196
980560
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 12317
54624156
00016717 00000-0 10270-3 0 9105
2 25544 51
6437 104
4835 0015507 275
4778 84
4605 15
51393749 41066
Satellite: ISS
Catalog Number: 25544
Epoch time: 12317
54624156 = yrday
fracday
Element set: 910
Inclination: 51
6437 deg
RA of node: 104
4835 deg
Eccentricity:
0015507
Arg of perigee: 275
4778 deg
Mean anomaly: 84
4605 deg
Mean motion: 15
51393749 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4106
Checksum: 315
Coasting Arc #12 (Orbit 4120)
---------------------------------------
Vector Time (GMT): 2012/318/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3499520
80 A = 6786538
28 meter
Y = 2955155
54 meter E =
0003407
Z = -5005195
37 I = 51
97648
XDOT = -2743
789644 Wp = 254
96192
YDOT = 6837
940233 meter/sec RA = 98
88117 deg
ZDOT = 2116
784928 TA = 35
56885
MA = 35
54614
Ha = 224
898 n
mi
Hp = 219
490
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11481367
47 X = 3490530
40
Y = 9695392
18 feet Y = 2994239
22 meter
Z = -16421244
65 Z = -4988216
10
XDOT = -9001
934528 XDOT = -2830
332175
YDOT = 22434
187115 feet/sec YDOT = 6806
773523 meter/sec
ZDOT = 6944
832441 ZDOT = 2103
245265
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14758706
63 X = -4498453
78
Y = 3209173
71 feet Y = 978156
15 meter
Z = -16351192
22 Z = -4983843
39
XDOT = -11948
643418 XDOT = -3641
946514
YDOT = -19821
077341 feet/sec YDOT = -6041
464373 meter/sec
ZDOT = 6887
957133 ZDOT = 2099
449334
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 12318
51243337
00016717 00000-0 10270-3 0 9112
2 25544 51
6451 99
6870 0015604 279
1195 80
8191 15
51475929 41216
Satellite: ISS
Catalog Number: 25544
Epoch time: 12318
51243337 = yrday
fracday
Element set: 911
Inclination: 51
6451 deg
RA of node: 99
6870 deg
Eccentricity:
0015604
Arg of perigee: 279
1195 deg
Mean anomaly: 80
8191 deg
Mean motion: 15
51475929 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4121
Checksum: 312
Coasting Arc #13 (Orbit 4136)
---------------------------------------
Vector Time (GMT): 2012/319/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3402031
66 A = 6788008
51 meter
Y = -3592581
64 meter E =
0010308
Z = 4657163
41 I = 51
98537
XDOT = 2775
437059 Wp = 312
60298
YDOT = -6485
522601 meter/sec RA = 93
93396 deg
ZDOT = -2972
951280 TA = 166
94337
MA = 166
91666
Ha = 224
957 n
mi
Hp = 219
654
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11161521
18 X = -3384229
88
Y = -11786685
18 feet Y = -3630526
00 meter
Z = 15279407
52 Z = 4640679
09
XDOT = 9105
764630 XDOT = 2862
195577
YDOT = -21277
961291 feet/sec YDOT = -6454
000678 meter/sec
ZDOT = -9753
777165 ZDOT = -2959
257562
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16179718
63 X = 4931578
24
Y = -1947650
85 feet Y = -593643
98 meter
Z = 15211481
12 Z = 4636459
45
XDOT = 11400
282086 XDOT = 3474
805980
YDOT = 18908
960129 feet/sec YDOT = 5763
451047 meter/sec
ZDOT = -9696
280929 ZDOT = -2955
426427
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 12319
54302016
00016717 00000-0 10270-3 0 9127
2 25544 51
6454 94
5693 0015541 283
0611 76
8805 15
51468250 41376
Satellite: ISS
Catalog Number: 25544
Epoch time: 12319
54302016 = yrday
fracday
Element set: 912
Inclination: 51
6454 deg
RA of node: 94
5693 deg
Eccentricity:
0015541
Arg of perigee: 283
0611 deg
Mean anomaly: 76
8805 deg
Mean motion: 15
51468250 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4137
Checksum: 297
Coasting Arc #14 (Orbit 4151)
---------------------------------------
Vector Time (GMT): 2012/320/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3335364
76 A = 6789609
83 meter
Y = 4182279
04 meter E =
0008047
Z = -4173103
30 I = 51
99367
XDOT = -2843
713074 Wp = 284
93975
YDOT = 6038
193579 meter/sec RA = 88
99003 deg
ZDOT = 3774
588519 TA = 23
74287
MA = 23
70576
Ha = 225
295 n
mi
Hp = 219
419
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10942797
77 X = 3308622
19
Y = 13721387
93 feet Y = 4219427
94 meter
Z = -13691283
79 Z = -4156964
55
XDOT = -9329
767302 XDOT = -2929
358573
YDOT = 19810
346389 feet/sec YDOT = 6005
914267 meter/sec
ZDOT = 12383
820602 ZDOT = 3760
565969
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17578725
59 X = -5357995
56
Y = 907825
37 feet Y = 276705
17 meter
Z = -13624860
42 Z = -4152857
46
XDOT = -10489
666338 XDOT = -3197
250300
YDOT = -17941
084802 feet/sec YDOT = -5468
442648 meter/sec
ZDOT = 12324
992721 ZDOT = 3756
657781
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 12320
50917367
00016717 00000-0 10270-3 0 9137
2 25544 51
6467 89
7726 0015701 287
1403 72
8029 15
51524061 41529
Satellite: ISS
Catalog Number: 25544
Epoch time: 12320
50917367 = yrday
fracday
Element set: 913
Inclination: 51
6467 deg
RA of node: 89
7726 deg
Eccentricity:
0015701
Arg of perigee: 287
1403 deg
Mean anomaly: 72
8029 deg
Mean motion: 15
51524061 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4152
Checksum: 300
Coasting Arc #15 (Orbit 4167)
---------------------------------------
Vector Time (GMT): 2012/321/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906518
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3312205
54 A = 6791467
06 meter
Y = -4725234
96 meter E =
0006619
Z = 3589296
69 I = 51
99898
XDOT = 2946
357537 Wp = 337
40135
YDOT = -5467
997583 meter/sec RA = 84
04804 deg
ZDOT = -4476
401816 TA = 160
51086
MA = 160
48555
Ha = 225
371 n
mi
Hp = 219
499
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10866816
06 X = -3276557
08
Y = -15502739
36 feet Y = -4762075
05 meter
Z = 11775907
78 Z = 3573292
12
XDOT = 9666
527351 XDOT = 3029
028555
YDOT = -17939
624617 feet/sec YDOT = -5434
587007 meter/sec
ZDOT = -14686
357665 ZDOT = -4461
887897
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18972442
66 X = 5782800
52
Y = -120198
13 feet Y = -36636
39 meter
Z = 11710106
53 Z = 3569240
47
XDOT = 9140
555872 XDOT = 2786
041430
YDOT = 16874
229506 feet/sec YDOT = 5143
265154 meter/sec
ZDOT = -14625
542854 ZDOT = -4457
865462
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 12321
53971859
00016717 00000-0 10270-3 0 9148
2 25544 51
6471 84
6555 0015613 290
9410 69
0070 15
51547302 41684
Satellite: ISS
Catalog Number: 25544
Epoch time: 12321
53971859 = yrday
fracday
Element set: 914
Inclination: 51
6471 deg
RA of node: 84
6555 deg
Eccentricity:
0015613
Arg of perigee: 290
9410 deg
Mean anomaly: 69
0070 deg
Mean motion: 15
51547302 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4168
Checksum: 306
INTERNATIONAL SPACE STATION ORBITAL DATA:
The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability The data normally contains past, current and predicted orbital data Careful attention to the orbit # / epoch times! These sources include:
NASA Orbital Flight Dynamics DOD C-Band Radar Network Goddard Space Flight Center (GSFC) NASA Johnson Space Center (JSC) DoD/ USSTRATCOM/ US Space Command with permission
By receiving this email, you agree not to transfer any data or information received under this agreement, including the analysis of tracking data, to any other entity without the express approval of the Aus-City Forum Admins and/ or DoD/ USSTRATCOM/ US Space Command
David Cottle
Director Of Engineering
IDB Communications
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