[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
July 22nd 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 11840 3 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 131 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 202 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 2319)
---------------------------------------
Vector Time (GMT): 2012/202/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923981
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5601516
08 A = 6782847
31 meter
Y = 1679498
96 meter E =
0004045
Z = -3440059
17 I = 51
40237
XDOT = 973
379471 Wp = 88
88073
YDOT = -6082
769089 meter/sec RA = 315
30399 deg
ZDOT = -4559
265903 TA = 131
56729
MA = 131
53260
Ha = 219
879 n
mi
Hp = 214
187
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18377677
43 X = -5603169
59
Y = 5510167
18 feet Y = 1616850
37 meter
Z = -11286283
36 Z = -3467274
39
XDOT = 3193
502201 XDOT = 1063
473322
YDOT = -19956
591500 feet/sec YDOT = -6071
380034 meter/sec
ZDOT = -14958
221468 ZDOT = -4554
319042
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13428163
33 X = 4092904
18
Y = 13610119
62 feet Y = 4148364
46 meter
Z = -11398694
48 Z = -3474322
08
XDOT = -18186
147828 XDOT = -5543
137858
YDOT = 5445
365676 feet/sec YDOT = 1659
747458 meter/sec
ZDOT = -14937
140624 ZDOT = -4552
840462
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 12202
52489029
00016717 00000-0 10270-3 0 9003
2 25544 51
6435 315
7564 0000977 259
4364 100
6679 15
54597329 23209
Satellite: ISS
Catalog Number: 25544
Epoch time: 12202
52489029 = yrday
fracday
Element set: 900
Inclination: 51
6435 deg
RA of node: 315
7564 deg
Eccentricity:
0000977
Arg of perigee: 259
4364 deg
Mean anomaly: 100
6679 deg
Mean motion: 15
54597329 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2320
Checksum: 316
Coasting Arc #2 (Orbit 2335)
---------------------------------------
Vector Time (GMT): 2012/203/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923981
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4958619
19 A = 6778634
79 meter
Y = -144130
00 meter E =
0007373
Z = 4615749
63 I = 51
36827
XDOT = -2541
601795 Wp = 118
56071
YDOT = 6618
446175 meter/sec RA = 310
29427 deg
ZDOT = 2930
035582 TA = 302
13255
MA = 302
20407
Ha = 219
688 n
mi
Hp = 214
183
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16268435
68 X = 4937440
53
Y = -472867
44 feet Y = -88798
34 meter
Z = 15143535
54 Z = 4639786
45
XDOT = -8338
588566 XDOT = -2629
654891
YDOT = 21714
062253 feet/sec YDOT = 6589
531892 meter/sec
ZDOT = 9612
977631 ZDOT = 2917
475375
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8218895
51 X = -2505119
35
Y = -13939983
13 feet Y = -4248906
86 meter
Z = 15242667
05 Z = 4645964
92
XDOT = 22054
722190 XDOT = 6722
279323
YDOT = -2524
352300 feet/sec YDOT = -769
422581 meter/sec
ZDOT = 9560
454993 ZDOT = 2914
026682
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 12203
55340018
00016717 00000-0 10270-3 0 9012
2 25544 51
6439 310
6255 0000967 268
5725 91
5317 15
54653429 23363
Satellite: ISS
Catalog Number: 25544
Epoch time: 12203
55340018 = yrday
fracday
Element set: 901
Inclination: 51
6439 deg
RA of node: 310
6255 deg
Eccentricity:
0000967
Arg of perigee: 268
5725 deg
Mean anomaly: 91
5317 deg
Mean motion: 15
54653429 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2336
Checksum: 299
Coasting Arc #3 (Orbit 2350)
---------------------------------------
Vector Time (GMT): 2012/204/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923981
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4020619
63 A = 6776144
05 meter
Y = -1569024
48 meter E =
0013503
Z = -5235741
87 I = 51
34053
XDOT = 3771
463989 Wp = 81
56845
YDOT = -6603
007356 meter/sec RA = 305
27298 deg
ZDOT = -917
505698 TA = 179
60782
MA = 179
60676
Ha = 219
836 n
mi
Hp = 214
087
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13191009
29 X = -3977342
04
Y = -5147718
10 feet Y = -1613743
33 meter
Z = -17177630
79 Z = -5255168
47
XDOT = 12373
569519 XDOT = 3849
476830
YDOT = -21663
409960 feet/sec YDOT = -6560
396268 meter/sec
ZDOT = -3010
189299 ZDOT = -898
995223
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2044531
48 X = 623173
20
Y = 13912911
08 feet Y = 4240655
30 meter
Z = -17257564
24 Z = -5260105
58
XDOT = -23942
729532 XDOT = -7297
743961
YDOT = -119
464163 feet/sec YDOT = -36
412677 meter/sec
ZDOT = -2933
144870 ZDOT = -894
022556
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 12204
51761899
00016717 00000-0 10270-3 0 9024
2 25544 51
6436 305
8159 0001013 280
3555 79
7484 15
54635605 23511
Satellite: ISS
Catalog Number: 25544
Epoch time: 12204
51761899 = yrday
fracday
Element set: 902
Inclination: 51
6436 deg
RA of node: 305
8159 deg
Eccentricity:
0001013
Arg of perigee: 280
3555 deg
Mean anomaly: 79
7484 deg
Mean motion: 15
54635605 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2351
Checksum: 309
Coasting Arc #4 (Orbit 2366)
---------------------------------------
Vector Time (GMT): 2012/205/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923981
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2890464
28 A = 6776220
95 meter
Y = 3273735
57 meter E =
0003627
Z = 5179575
64 I = 51
32443
XDOT = -4621
583634 Wp = 42
43825
YDOT = 6001
622011 meter/sec RA = 300
24540 deg
ZDOT = -1211
104172 TA = 59
24694
MA = 59
21123
Ha = 219
680 n
mi
Hp = 214
125
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9483150
53 X = 2828481
01
Y = 10740602
25 feet Y = 3305711
78 meter
Z = 16993358
40 Z = 5193466
76
XDOT = -15162
675963 XDOT = -4682
468328
YDOT = 19690
360928 feet/sec YDOT = 5949
600210 meter/sec
ZDOT = -3973
438885 ZDOT = -1233
702984
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4418603
40 X = 1346790
31
Y = -13558341
94 feet Y = -4132582
62 meter
Z = 17050285
00 Z = 5196926
87
XDOT = 23676
875928 XDOT = 7216
711783
YDOT = 2588
544368 feet/sec YDOT = 788
988323 meter/sec
ZDOT = -4067
265118 ZDOT = -1239
702408
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 12205
54610530
00016717 00000-0 10270-3 0 9034
2 25544 51
6435 300
6844 0001000 290
4238 69
6807 15
54689899 23678
Satellite: ISS
Catalog Number: 25544
Epoch time: 12205
54610530 = yrday
fracday
Element set: 903
Inclination: 51
6435 deg
RA of node: 300
6844 deg
Eccentricity:
0001000
Arg of perigee: 290
4238 deg
Mean anomaly: 69
6807 deg
Mean motion: 15
54689899 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2367
Checksum: 306
Coasting Arc #5 (Orbit 2381)
---------------------------------------
Vector Time (GMT): 2012/206/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923981
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1707335
00 A = 6779104
06 meter
Y = -4797992
80 meter E =
0008624
Z = -4483074
88 I = 51
31917
XDOT = 5070
556934 Wp = 109
75323
YDOT = -4779
051923 meter/sec RA = 295
22266 deg
ZDOT = 3185
842053 TA = 192
42203
MA = 192
44330
Ha = 219
789 n
mi
Hp = 214
003
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5601492
77 X = -1631778
40
Y = -15741446
20 feet Y = -4816662
66 meter
Z = -14708250
93 Z = -4491185
61
XDOT = 16635
685480 XDOT = 5108
144467
YDOT = -15679
304209 feet/sec YDOT = -4722
139756 meter/sec
ZDOT = 10452
237706 ZDOT = 3210
565483
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10472954
29 X = -3192156
47
Y = 12981417
38 feet Y = 3956736
02 meter
Z = -14741184
70 Z = -4493113
10
XDOT = -21111
909878 XDOT = -6434
910131
YDOT = -5054
869924 feet/sec YDOT = -1540
724353 meter/sec
ZDOT = 10554
685887 ZDOT = 3217
068258
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 12206
51030145
00016717 00000-0 10270-3 0 9041
2 25544 51
6430 295
8746 0000912 295
4223 64
6836 15
54703695 23824
Satellite: ISS
Catalog Number: 25544
Epoch time: 12206
51030145 = yrday
fracday
Element set: 904
Inclination: 51
6430 deg
RA of node: 295
8746 deg
Eccentricity:
0000912
Arg of perigee: 295
4223 deg
Mean anomaly: 64
6836 deg
Mean motion: 15
54703695 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2382
Checksum: 299
Coasting Arc #6 (Orbit 2397)
---------------------------------------
Vector Time (GMT): 2012/207/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923981
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 528325
68 A = 6783351
63 meter
Y = 5957354
11 meter E =
0012061
Z = 3189994
65 I = 51
32081
XDOT = -5186
661523 Wp = 91
06110
YDOT = 3024
953627 meter/sec RA = 290
20924 deg
ZDOT = -4774
673215 TA = 51
86463
MA = 51
75599
Ha = 219
825 n
mi
Hp = 214
040
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1733351
98 X = 446173
88
Y = 19545125
02 feet Y = 5962802
69 meter
Z = 10465861
71 Z = 3192361
95
XDOT = -17016
606045 XDOT = -5196
907549
YDOT = 9924
388541 feet/sec YDOT = 2966
896091 meter/sec
ZDOT = -15664
938368 ZDOT = -4799
894375
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15526339
53 X = 4732428
29
Y = -11989908
94 feet Y = -3654524
24 meter
Z = 10474996
29 Z = 3192778
87
XDOT = 16632
137934 XDOT = 5069
475642
YDOT = 7716
724423 feet/sec YDOT = 2352
057604 meter/sec
ZDOT = -15769
249419 ZDOT = -4806
467223
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 12207
53876529
00016717 00000-0 10270-3 0 9059
2 25544 51
6426 290
7429 0000948 307
5975 52
5092 15
54697022 23982
Satellite: ISS
Catalog Number: 25544
Epoch time: 12207
53876529 = yrday
fracday
Element set: 905
Inclination: 51
6426 deg
RA of node: 290
7429 deg
Eccentricity:
0000948
Arg of perigee: 307
5975 deg
Mean anomaly: 52
5092 deg
Mean motion: 15
54697022 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2398
Checksum: 335
Coasting Arc #7 (Orbit 2412)
---------------------------------------
Vector Time (GMT): 2012/208/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923981
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 539955
56 A = 6786772
69 meter
Y = -6590754
84 meter E =
0008504
Z = -1508747
80 I = 51
32241
XDOT = 5005
404245 Wp = 29
52097
YDOT = -898
922605 meter/sec RA = 285
20712 deg
ZDOT = 5739
271038 TA = 313
92431
MA = 313
99446
Ha = 219
848 n
mi
Hp = 214
099
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1771507
73 X = 620943
73
Y = -21623211
42 feet Y = -6584263
79 meter
Z = -4949959
97 Z = -1505928
45
XDOT = 16421
929937 XDOT = 4987
204208
YDOT = -2949
221146 feet/sec YDOT = -843
051211 meter/sec
ZDOT = 18829
629390 ZDOT = 5763
542695
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18974722
73 X = -5783495
49
Y = 10525357
78 feet Y = 3208129
05 meter
Z = -4937646
83 Z = -1504994
75
XDOT = -10749
405191 XDOT = -3276
418702
YDOT = -10530
854100 feet/sec YDOT = -3209
804330 meter/sec
ZDOT = 18929
802532 ZDOT = 5769
803812
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 12208
50293837
00016717 00000-0 10270-3 0 9063
2 25544 51
6425 285
9320 0001191 314
8234 45
2822 15
54676274 24131
Satellite: ISS
Catalog Number: 25544
Epoch time: 12208
50293837 = yrday
fracday
Element set: 906
Inclination: 51
6425 deg
RA of node: 285
9320 deg
Eccentricity:
0001191
Arg of perigee: 314
8234 deg
Mean anomaly: 45
2822 deg
Mean motion: 15
54676274 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2413
Checksum: 298
Coasting Arc #8 (Orbit 2428)
---------------------------------------
Vector Time (GMT): 2012/209/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923981
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1516566
14 A = 6787517
69 meter
Y = 6598770
33 meter E =
0010211
Z = -403025
42 I = 51
31766
XDOT = -4601
082010 Wp = 137
39238
YDOT = -1416
144314 meter/sec RA = 280
21166 deg
ZDOT = -5969
260517 TA = 46
97304
MA = 46
88755
Ha = 219
837 n
mi
Hp = 213
949
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4975610
70 X = -1588284
44
Y = 21649508
94 feet Y = 6581410
18 meter
Z = -1322261
87 Z = -410566
40
XDOT = -15095
413417 XDOT = -4555
907256
YDOT = -4646
142764 feet/sec YDOT = -1467
343351 meter/sec
ZDOT = -19584
188049 ZDOT = -5991
502655
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20617307
90 X = 6284155
45
Y = -8264351
37 feet Y = -2518974
30 meter
Z = -1354041
06 Z = -412711
71
XDOT = 4118
944622 XDOT = 1255
454321
YDOT = 13448
812741 feet/sec YDOT = 4099
198123 meter/sec
ZDOT = -19675
755513 ZDOT = -5997
170280
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 12209
53137943
00016717 00000-0 10270-3 0 9073
2 25544 51
6418 280
8003 0001032 321
5846 38
5233 15
54726512 24292
Satellite: ISS
Catalog Number: 25544
Epoch time: 12209
53137943 = yrday
fracday
Element set: 907
Inclination: 51
6418 deg
RA of node: 280
8003 deg
Eccentricity:
0001032
Arg of perigee: 321
5846 deg
Mean anomaly: 38
5233 deg
Mean motion: 15
54726512 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2429
Checksum: 289
Coasting Arc #9 (Orbit 2444)
---------------------------------------
Vector Time (GMT): 2012/210/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923981
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2341978
32 A = 6785398
90 meter
Y = -5955045
49 meter E =
0013648
Z = 2236306
49 I = 51
30658
XDOT = 4031
696931 Wp = 67
19906
YDOT = 3630
682211 meter/sec RA = 275
21325 deg
ZDOT = 5424
616413 TA = 317
80545
MA = 317
91042
Ha = 219
817 n
mi
Hp = 213
891
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7683655
91 X = 2397531
42
Y = -19537550
83 feet Y = -5928545
66 meter
Z = 7336963
55 Z = 2247817
92
XDOT = 13227
352137 XDOT = 3964
446904
YDOT = 11911
687045 feet/sec YDOT = 3675
390553 meter/sec
ZDOT = 17797
297943 ZDOT = 5444
039100
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20318534
92 X = -6193089
44
Y = 5215719
93 feet Y = 1589751
44 meter
Z = 7385045
65 Z = 2250961
91
XDOT = 2383
625214 XDOT = 726
528965
YDOT = -16124
995951 feet/sec YDOT = -4914
898766 meter/sec
ZDOT = 17877
017786 ZDOT = 5448
915021
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 12210
55980784
00016717 00000-0 10270-3 0 9087
2 25544 51
6421 275
6683 0001110 328
5289 31
5798 15
54742276 24459
Satellite: ISS
Catalog Number: 25544
Epoch time: 12210
55980784 = yrday
fracday
Element set: 908
Inclination: 51
6421 deg
RA of node: 275
6683 deg
Eccentricity:
0001110
Arg of perigee: 328
5289 deg
Mean anomaly: 31
5798 deg
Mean motion: 15
54742276 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2445
Checksum: 320
Coasting Arc #10 (Orbit 2459)
---------------------------------------
Vector Time (GMT): 2012/211/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923981
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3069678
04 A = 6781300
97 meter
Y = 4701598
88 meter E =
0006063
Z = -3809299
26 I = 51
29063
XDOT = -3309
046725 Wp = 65
19886
YDOT = -5523
578361 meter/sec RA = 270
20488 deg
ZDOT = -4153
600687 TA = 160
81099
MA = 160
78815
Ha = 219
870 n
mi
Hp = 213
780
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10071122
18 X = -3103519
67
Y = 15425193
18 feet Y = 4667083
05 meter
Z = -12497700
97 Z = -3824293
09
XDOT = -10856
452511 XDOT = -3226
858006
YDOT = -18121
976249 feet/sec YDOT = -5560
122160 meter/sec
ZDOT = -13627
298842 ZDOT = -4169
476679
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18339106
17 X = 5589759
56
Y = -1216491
98 feet Y = -370786
76 meter
Z = -12560013
87 Z = -3828292
23
XDOT = -8168
354405 XDOT = -2489
714423
YDOT = 18136
123293 feet/sec YDOT = 5527
890380 meter/sec
ZDOT = -13692
210079 ZDOT = -4173
385632
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 12211
52394978
00016717 00000-0 10270-3 0 9090
2 25544 51
6414 270
8573 0001127 334
7191 25
3907 15
54753329 24606
Satellite: ISS
Catalog Number: 25544
Epoch time: 12211
52394978 = yrday
fracday
Element set: 909
Inclination: 51
6414 deg
RA of node: 270
8573 deg
Eccentricity:
0001127
Arg of perigee: 334
7191 deg
Mean anomaly: 25
3907 deg
Mean motion: 15
54753329 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2460
Checksum: 310
Coasting Arc #11 (Orbit 2475)
---------------------------------------
Vector Time (GMT): 2012/212/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923981
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3659900
35 A = 6777264
88 meter
Y = -2978901
45 meter E =
0005895
Z = 4860614
85 I = 51
27840
XDOT = 2469
126177 Wp = 113
76185
YDOT = 6873
716759 meter/sec RA = 265
18356 deg
ZDOT = 2348
881624 TA = 313
10888
MA = 313
15819
Ha = 219
722 n
mi
Hp = 213
770
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12007547
07 X = 3669327
68
Y = -9773298
71 feet Y = -2937921
98 meter
Z = 15946899
12 Z = 4878416
74
XDOT = 8100
807666 XDOT = 2380
669221
YDOT = 22551
564169 feet/sec YDOT = 6900
833217 meter/sec
ZDOT = 7706
304542 ZDOT = 2360
662197
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15016613
63 X = -4577063
84
Y = -3441398
32 feet Y = -1048938
21 meter
Z = 16020619
16 Z = 4883084
72
XDOT = 12659
793697 XDOT = 3858
705119
YDOT = -19073
468000 feet/sec YDOT = -5813
593047 meter/sec
ZDOT = 7754
203888 ZDOT = 2363
481345
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 12212
55235507
00016717 00000-0 10270-3 0 9108
2 25544 51
6414 265
7256 0001225 339
1385 20
9718 15
54792571 24760
Satellite: ISS
Catalog Number: 25544
Epoch time: 12212
55235507 = yrday
fracday
Element set: 910
Inclination: 51
6414 deg
RA of node: 265
7256 deg
Eccentricity:
0001225
Arg of perigee: 339
1385 deg
Mean anomaly: 20
9718 deg
Mean motion: 15
54792571 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2476
Checksum: 302
Coasting Arc #12 (Orbit 2490)
---------------------------------------
Vector Time (GMT): 2012/213/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923981
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4136623
49 A = 6775485
00 meter
Y = 971788
12 meter E =
0014634
Z = -5290104
60 I = 51
27556
XDOT = -1482
386942 Wp = 83
33665
YDOT = -7510
846693 meter/sec RA = 260
15220 deg
ZDOT = -219
434286 TA = 184
55207
MA = 184
56539
Ha = 219
918 n
mi
Hp = 213
591
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13571599
37 X = -4121485
23
Y = 3188281
25 feet Y = 925614
96 meter
Z = -17355986
23 Z = -5310162
82
XDOT = -4863
474220 XDOT = -1397
222996
YDOT = -24641
885475 feet/sec YDOT = -7526
947466 meter/sec
ZDOT = -719
928760 ZDOT = -226
429322
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10907654
94 X = 3324653
23
Y = 8514366
66 feet Y = 2595178
96 meter
Z = -17438816
73 Z = -5315351
34
XDOT = -15569
586015 XDOT = -4745
609817
YDOT = 18406
255408 feet/sec YDOT = 5610
226649 meter/sec
ZDOT = -748
043898 ZDOT = -228
003780
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 12213
51647643
00016717 00000-0 10270-3 0 9114
2 25544 51
6411 260
9141 0001294 345
9683 14
1433 15
54777620 24913
Satellite: ISS
Catalog Number: 25544
Epoch time: 12213
51647643 = yrday
fracday
Element set: 911
Inclination: 51
6411 deg
RA of node: 260
9141 deg
Eccentricity:
0001294
Arg of perigee: 345
9683 deg
Mean anomaly: 14
1433 deg
Mean motion: 15
54777620 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2491
Checksum: 291
Coasting Arc #13 (Orbit 2506)
---------------------------------------
Vector Time (GMT): 2012/214/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923981
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4438393
01 A = 6776534
85 meter
Y = 1104535
56 meter E =
0006484
Z = 4997580
12 I = 51
28521
XDOT = 354
541872 Wp = 45
17976
YDOT = 7412
014981 meter/sec RA = 255
12053 deg
ZDOT = -1946
981140 TA = 63
83477
MA = 63
76810
Ha = 219
745 n
mi
Hp = 213
601
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14561656
87 X = 4401435
49
Y = 3623804
32 feet Y = 1153961
44 meter
Z = 16396260
24 Z = 5019051
40
XDOT = 1163
195118 XDOT = 281
090601
YDOT = 24317
634451 feet/sec YDOT = 7415
569133 meter/sec
ZDOT = -6387
733398 ZDOT = -1945
436732
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6446945
29 X = -1965028
92
Y = -13442540
73 feet Y = -4097286
42 meter
Z = 16484724
85 Z = 5024544
13
XDOT = 16963
203208 XDOT = 5170
384338
YDOT = -15986
043639 feet/sec YDOT = -4872
546101 meter/sec
ZDOT = -6382
074490 ZDOT = -1945
256304
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 12214
54485909
00016717 00000-0 10270-3 0 9124
2 25544 51
6404 255
7822 0001368 351
9231 8
1900 15
54839025 25079
Satellite: ISS
Catalog Number: 25544
Epoch time: 12214
54485909 = yrday
fracday
Element set: 912
Inclination: 51
6404 deg
RA of node: 255
7822 deg
Eccentricity:
0001368
Arg of perigee: 351
9231 deg
Mean anomaly: 8
1900 deg
Mean motion: 15
54839025 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2507
Checksum: 297
Coasting Arc #14 (Orbit 2521)
---------------------------------------
Vector Time (GMT): 2012/215/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923981
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4539232
48 A = 6780190
31 meter
Y = -2995866
14 meter E =
0007076
Z = -4055371
53 I = 51
30662
XDOT = 900
261312 Wp = 97
56773
YDOT = -6565
508274 meter/sec RA = 250
09659 deg
ZDOT = 3847
399990 TA = 212
44780
MA = 212
49132
Ha = 219
943 n
mi
Hp = 213
398
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14892495
00 X = -4485695
14
Y = -9828957
14 feet Y = -3046327
13 meter
Z = -13305024
72 Z = -4077292
46
XDOT = 2953
613227 XDOT = 954
921940
YDOT = -21540
381478 feet/sec YDOT = -6555
135540 meter/sec
ZDOT = 12622
703378 ZDOT = 3851
905782
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2199554
23 X = 670424
13
Y = 17639436
75 feet Y = 5376500
32 meter
Z = -13395175
28 Z = -4082849
43
XDOT = -16923
517572 XDOT = -5158
288156
YDOT = 11698
343808 feet/sec YDOT = 3565
655193 meter/sec
ZDOT = 12641
907389 ZDOT = 3853
253372
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 12215
50895941
00016717 00000-0 10270-3 0 9133
2 25544 51
6407 250
9703 0001437 3
1289 356
9873 15
54841159 25224
Satellite: ISS
Catalog Number: 25544
Epoch time: 12215
50895941 = yrday
fracday
Element set: 913
Inclination: 51
6407 deg
RA of node: 250
9703 deg
Eccentricity:
0001437
Arg of perigee: 3
1289 deg
Mean anomaly: 356
9873 deg
Mean motion: 15
54841159 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2522
Checksum: 311
Coasting Arc #15 (Orbit 2537)
---------------------------------------
Vector Time (GMT): 2012/216/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923981
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4347195
71 A = 6784404
86 meter
Y = 4541352
32 meter E =
0013556
Z = 2536210
48 I = 51
33125
XDOT = -2261
643449 Wp = 97
57473
YDOT = 5111
603417 meter/sec RA = 245
08644 deg
ZDOT = -5253
881570 TA = 53
79345
MA = 53
66818
Ha = 219
941 n
mi
Hp = 213
395
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14262453
12 X = 4283770
23
Y = 14899449
88 feet Y = 4589610
68 meter
Z = 8320900
52 Z = 2557174
51
XDOT = -7420
090057 XDOT = -2293
112789
YDOT = 16770
352418 feet/sec YDOT = 5086
136475 meter/sec
ZDOT = -17237
144258 ZDOT = -5264
944599
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1683556
57 X = 513148
04
Y = -20521622
85 feet Y = -6254990
65 meter
Z = 8406972
93 Z = 2562445
35
XDOT = 15893
435336 XDOT = 4844
319090
YDOT = -5806
272417 feet/sec YDOT = -1769
751833 meter/sec
ZDOT = -17283
254644 ZDOT = -5267
936016
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 12216
53732030
00016717 00000-0 10270-3 0 9147
2 25544 51
6398 245
8375 0001502 6
8626 353
2547 15
54865011 25387
Satellite: ISS
Catalog Number: 25544
Epoch time: 12216
53732030 = yrday
fracday
Element set: 914
Inclination: 51
6398 deg
RA of node: 245
8375 deg
Eccentricity:
0001502
Arg of perigee: 6
8626 deg
Mean anomaly: 353
2547 deg
Mean motion: 15
54865011 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2538
Checksum: 298
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
The following information is a reminder of your current mailing list subscription:
You are subscribed to the following list: [list_name]
using the following email: example@example.com
You may automatically unsubscribe from this list at any time by visiting the following URL:
https://aus-city com/cgi-bin/dada/mail cgi/u/ISSTLE_LIST/example/example com/
If the above URL is inoperable, make sure that you have copied the entire address Some mail readers will wrap a long URL and thus break this automatic unsubscribe mechanism
You may also change your subscription by visiting this list's main screen:
<[program_url]/list/[list]>
If you're still having trouble, please contact the list owner at:
<mailto:[list_owner_email]>
The following physical address is associated with this mailing list:
[physical_address]
- This mailing list is a public mailing list - anyone may join or leave, at any time.
-
This mailing list is announce-only.
ISS TLE list
Privacy Policy:
Private list