[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
October 31st 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14531 28 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 3884)
---------------------------------------
Vector Time (GMT): 2012/303/07:11:27
081
Vector Time (MET): N/A
Weight (LBS) : 891465
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3732362
91 A = 6790200
35 meter
Y = 3763914
56 meter E =
0015189
Z = -4250064
42 I = 51
67179
XDOT = -6374
338973 Wp = 194
44815
YDOT = -2216
147198 meter/sec RA = 174
09414 deg
ZDOT = 3618
062975 TA = 112
66819
MA = 112
50752
Ha = 227
929 n
mi
Hp = 218
956
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12245285
13 X = -3753527
97
Y = 12348801
06 feet Y = 3722058
37 meter
Z = -13943780
90 Z = -4268248
18
XDOT = -20913
185608 XDOT = -6366
660000
YDOT = -7270
824141 feet/sec YDOT = -2287
385900 meter/sec
ZDOT = 11870
285350 ZDOT = 3587
114666
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17038667
49 X = 5193385
85
Y = -3163768
90 feet Y = -964316
76 meter
Z = -14019390
06 Z = -4273110
09
XDOT = 12814
460345 XDOT = 3905
847513
YDOT = 16731
676464 feet/sec YDOT = 5099
814986 meter/sec
ZDOT = 11742
370295 ZDOT = 3579
074466
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 12303
30918482
00016717 00000-0 10270-3 0 9001
2 25544 51
6461 175
1528 0016490 223
8839 136
1003 15
51184659 38852
Satellite: ISS
Catalog Number: 25544
Epoch time: 12303
30918482 = yrday
fracday
Element set: 900
Inclination: 51
6461 deg
RA of node: 175
1528 deg
Eccentricity:
0016490
Arg of perigee: 223
8839 deg
Mean anomaly: 136
1003 deg
Mean motion: 15
51184659 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3885
Checksum: 307
Coasting Arc #2 (Orbit 3900)
---------------------------------------
Vector Time (GMT): 2012/304/07:11:27
081
Vector Time (MET): N/A
Weight (LBS) : 891465
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4144575
07 A = 6791673
75 meter
Y = -3828638
43 meter E =
0009709
Z = 3772728
05 I = 51
70762
XDOT = 5960
237303 Wp = 185
09809
YDOT = 2273
412088 meter/sec RA = 169
13421 deg
ZDOT = -4250
864484 TA = 309
81306
MA = 309
89848
Ha = 227
576 n
mi
Hp = 219
068
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13597687
25 X = 4168752
10
Y = -12561149
71 feet Y = -3782155
88 meter
Z = 12377716
71 Z = 3792921
65
XDOT = 19554
584327 XDOT = 5955
022867
YDOT = 7458
701077 feet/sec YDOT = 2340
033864 meter/sec
ZDOT = -13946
405788 ZDOT = -4221
921869
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18230309
56 X = -5556598
35
Y = 2872314
86 feet Y = 875481
57 meter
Z = 12461664
10 Z = 3798315
22
XDOT = -11921
553137 XDOT = -3633
689396
YDOT = -15822
150101 feet/sec YDOT = -4822
591351 meter/sec
ZDOT = -13826
789486 ZDOT = -4214
405435
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 12304
33995422
00016717 00000-0 10270-3 0 9015
2 25544 51
6464 170
0378 0016465 227
8181 132
1573 15
51226418 39015
Satellite: ISS
Catalog Number: 25544
Epoch time: 12304
33995422 = yrday
fracday
Element set: 901
Inclination: 51
6464 deg
RA of node: 170
0378 deg
Eccentricity:
0016465
Arg of perigee: 227
8181 deg
Mean anomaly: 132
1573 deg
Mean motion: 15
51226418 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3901
Checksum: 294
Coasting Arc #3 (Orbit 3915)
---------------------------------------
Vector Time (GMT): 2012/305/07:11:27
081
Vector Time (MET): N/A
Weight (LBS) : 891465
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4554547
98 A = 6793359
23 meter
Y = 3905383
33 meter E =
0012657
Z = -3190039
86 I = 51
74250
XDOT = -5447
844803 Wp = 222
08256
YDOT = -2403
119783 meter/sec RA = 164
17670 deg
ZDOT = 4815
847142 TA = 101
20008
MA = 101
05779
Ha = 227
329 n
mi
Hp = 219
175
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14942742
72 X = -4582383
36
Y = 12812937
43 feet Y = 3854295
82 meter
Z = -10466010
04 Z = -3212233
95
XDOT = -17873
506573 XDOT = -5443
962655
YDOT = -7884
251257 feet/sec YDOT = -2464
019175 meter/sec
ZDOT = 15800
023431 ZDOT = 4789
390515
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19453728
01 X = 5929496
30
Y = -2658924
42 feet Y = -810440
16 meter
Z = -10558261
18 Z = -3218158
01
XDOT = 10597
852176 XDOT = 3230
225343
YDOT = 14970
570610 feet/sec YDOT = 4563
029922 meter/sec
ZDOT = 15690
701985 ZDOT = 4782
525965
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 12305
30628267
00016717 00000-0 10270-3 0 9024
2 25544 51
6458 165
2411 0016473 231
6765 128
2906 15
51243613 39160
Satellite: ISS
Catalog Number: 25544
Epoch time: 12305
30628267 = yrday
fracday
Element set: 902
Inclination: 51
6458 deg
RA of node: 165
2411 deg
Eccentricity:
0016473
Arg of perigee: 231
6765 deg
Mean anomaly: 128
2906 deg
Mean motion: 15
51243613 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3916
Checksum: 298
Coasting Arc #4 (Orbit 3931)
---------------------------------------
Vector Time (GMT): 2012/306/07:11:27
081
Vector Time (MET): N/A
Weight (LBS) : 891465
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4852000
61 A = 6794786
82 meter
Y = -3996952
73 meter E =
0012479
Z = 2559727
81 I = 51
77710
XDOT = 4914
086549 Wp = 181
69882
YDOT = 2588
288120 meter/sec RA = 159
22395 deg
ZDOT = -5285
991878 TA = 329
61305
MA = 329
68532
Ha = 226
963 n
mi
Hp = 219
273
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15918637
16 X = 4883899
85
Y = -13113361
98 feet Y = -3942516
25 meter
Z = 8398057
11 Z = 2583376
73
XDOT = 16122
331196 XDOT = 4910
457358
YDOT = 8491
758925 feet/sec YDOT = 2643
220175 meter/sec
ZDOT = -17342
493037 ZDOT = -5262
127686
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20402889
75 X = -6218800
80
Y = 2724820
85 feet Y = 830525
40 meter
Z = 8496356
62 Z = 2589689
50
XDOT = -9074
208408 XDOT = -2765
818723
YDOT = -14306
571704 feet/sec YDOT = -4360
643055 meter/sec
ZDOT = -17243
914115 ZDOT = -5255
945022
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 12306
33701457
00016717 00000-0 10270-3 0 9032
2 25544 51
6464 160
1254 0016426 235
4881 124
4719 15
51279261 39321
Satellite: ISS
Catalog Number: 25544
Epoch time: 12306
33701457 = yrday
fracday
Element set: 903
Inclination: 51
6464 deg
RA of node: 160
1254 deg
Eccentricity:
0016426
Arg of perigee: 235
4881 deg
Mean anomaly: 124
4719 deg
Mean motion: 15
51279261 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3932
Checksum: 297
Coasting Arc #5 (Orbit 3946)
---------------------------------------
Vector Time (GMT): 2012/307/07:11:27
081
Vector Time (MET): N/A
Weight (LBS) : 891465
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5118707
62 A = 6796077
41 meter
Y = 4073312
03 meter E =
0010070
Z = -1840288
04 I = 51
80934
XDOT = -4312
816396 Wp = 254
08466
YDOT = -2854
695681 meter/sec RA = 154
27381 deg
ZDOT = 5648
960365 TA = 85
76059
MA = 85
64551
Ha = 226
697 n
mi
Hp = 219
319
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16793660
16 X = -5154935
89
Y = 13363884
60 feet Y = 4015868
88 meter
Z = -6037690
41 Z = -1865243
06
XDOT = -14149
660091 XDOT = -4308
016067
YDOT = -9365
799477 feet/sec YDOT = -2902
897463 meter/sec
ZDOT = 18533
334532 ZDOT = 5628
020059
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21244627
34 X = 6475362
41
Y = -2832467
82 feet Y = -863336
19 meter
Z = -6141422
80 Z = -1871905
67
XDOT = 7201
837429 XDOT = 2195
120048
YDOT = 13821
048327 feet/sec YDOT = 4212
655530 meter/sec
ZDOT = 18446
880789 ZDOT = 5622
609264
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
30330769
00016717 00000-0 10270-3 0 9045
2 25544 51
6460 155
3284 0016444 239
4107 120
5422 15
51301659 39472
Satellite: ISS
Catalog Number: 25544
Epoch time: 12307
30330769 = yrday
fracday
Element set: 904
Inclination: 51
6460 deg
RA of node: 155
3284 deg
Eccentricity:
0016444
Arg of perigee: 239
4107 deg
Mean anomaly: 120
5422 deg
Mean motion: 15
51301659 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3947
Checksum: 291
Coasting Arc #6 (Orbit 3962)
---------------------------------------
Vector Time (GMT): 2012/308/07:11:27
081
Vector Time (MET): N/A
Weight (LBS) : 891465
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5271668
32 A = 6796957
31 meter
Y = -4131638
29 meter E =
0015158
Z = 1100014
11 I = 51
84014
XDOT = 3720
875014 Wp = 192
32237
YDOT = 3184
296186 meter/sec RA = 149
32754 deg
ZDOT = -5900
994441 TA = 335
78307
MA = 335
85424
Ha = 226
381 n
mi
Hp = 219
386
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17295499
74 X = 5312133
63
Y = -13555243
74 feet Y = -4072460
96 meter
Z = 3608970
16 Z = 1125722
42
XDOT = 12207
595190 XDOT = 3713
657293
YDOT = 10447
165964 feet/sec YDOT = 3225
865021 meter/sec
ZDOT = -19360
217981 ZDOT = -5882
935733
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21736024
02 X = -6625140
12
Y = 3105054
58 feet Y = 946420
64 meter
Z = 3715845
22 Z = 1132589
62
XDOT = -5227
144520 XDOT = -1593
233650
YDOT = -13623
736767 feet/sec YDOT = -4152
514967 meter/sec
ZDOT = -19285
723432 ZDOT = -5878
288502
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
33400226
00016717 00000-0 10270-3 0 9056
2 25544 51
6468 150
2124 0016417 243
0399 116
9076 15
51322919 39635
Satellite: ISS
Catalog Number: 25544
Epoch time: 12308
33400226 = yrday
fracday
Element set: 905
Inclination: 51
6468 deg
RA of node: 150
2124 deg
Eccentricity:
0016417
Arg of perigee: 243
0399 deg
Mean anomaly: 116
9076 deg
Mean motion: 15
51322919 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3963
Checksum: 295
Coasting Arc #7 (Orbit 3977)
---------------------------------------
Vector Time (GMT): 2012/309/07:11:27
081
Vector Time (MET): N/A
Weight (LBS) : 891465
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5379760
36 A = 6797343
69 meter
Y = 4141342
80 meter E =
0007647
Z = -297646
10 I = 51
86745
XDOT = -3101
217408 Wp = 285
54731
YDOT = -3587
165794 meter/sec RA = 144
38320 deg
ZDOT = 6015
332078 TA = 71
26063
MA = 71
17767
Ha = 226
047 n
mi
Hp = 219
379
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17650132
42 X = -5424223
96
Y = 13587082
68 feet Y = 4080934
35 meter
Z = -976529
22 Z = -323889
19
XDOT = -10174
597794 XDOT = -3090
096129
YDOT = -11768
916648 feet/sec YDOT = -3621
783397 meter/sec
ZDOT = 19735
341462 ZDOT = 6000
293225
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 22019176
02 X = 6711444
85
Y = -3326691
90 feet Y = -1013975
69 meter
Z = -1085637
03 Z = -330902
17
XDOT = 3054
931010 XDOT = 931
142972
YDOT = 13678
238825 feet/sec YDOT = 4169
127194 meter/sec
ZDOT = 19673
389304 ZDOT = 5996
449060
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
30025976
00016717 00000-0 10270-3 0 9060
2 25544 51
6468 145
4152 0016409 247
2051 112
7367 15
51357702 39785
Satellite: ISS
Catalog Number: 25544
Epoch time: 12309
30025976 = yrday
fracday
Element set: 906
Inclination: 51
6468 deg
RA of node: 145
4152 deg
Eccentricity:
0016409
Arg of perigee: 247
2051 deg
Mean anomaly: 112
7367 deg
Mean motion: 15
51357702 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3978
Checksum: 309
Coasting Arc #8 (Orbit 3993)
---------------------------------------
Vector Time (GMT): 2012/310/07:11:27
081
Vector Time (MET): N/A
Weight (LBS) : 891465
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5386091
54 A = 6797279
84 meter
Y = -4100869
97 meter E =
0015967
Z = -492872
49 I = 51
89223
XDOT = 2522
332513 Wp = 210
92334
YDOT = 4043
682801 meter/sec RA = 139
44143 deg
ZDOT = -6008
061502 TA = 334
37175
MA = 334
45080
Ha = 225
833 n
mi
Hp = 219
375
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17670904
00 X = 5433942
32
Y = -13454297
82 feet Y = -4040371
79 meter
Z = -1617035
72 Z = -466590
45
XDOT = 8275
369138 XDOT = 2506
114007
YDOT = 13266
675856 feet/sec YDOT = 4071
798409 meter/sec
ZDOT = -19711
487869 ZDOT = -5995
847331
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21928766
45 X = -6683888
01
Y = 3570666
62 feet Y = 1088339
19 meter
Z = -1507754
81 Z = -459563
67
XDOT = -919
224369 XDOT = -280
179588
YDOT = -14055
699791 feet/sec YDOT = -4284
177296 meter/sec
ZDOT = -19661
278483 ZDOT = -5992
757682
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
33091655
00016717 00000-0 10270-3 0 9073
2 25544 51
6476 140
2991 0016466 250
7057 109
2314 15
51368468 39948
Satellite: ISS
Catalog Number: 25544
Epoch time: 12310
33091655 = yrday
fracday
Element set: 907
Inclination: 51
6476 deg
RA of node: 140
2991 deg
Eccentricity:
0016466
Arg of perigee: 250
7057 deg
Mean anomaly: 109
2314 deg
Mean motion: 15
51368468 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3994
Checksum: 315
Coasting Arc #9 (Orbit 4009)
---------------------------------------
Vector Time (GMT): 2012/311/07:11:27
081
Vector Time (MET): N/A
Weight (LBS) : 891465
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5350138
86 A = 6796538
49 meter
Y = 3979448
80 meter E =
0004959
Z = 1310073
29 I = 51
91275
XDOT = -1955
112292 Wp = 305
45681
YDOT = -4546
937327 meter/sec RA = 134
49999 deg
ZDOT = 5845
650591 TA = 68
72187
MA = 68
66892
Ha = 225
439 n
mi
Hp = 219
347
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17552949
00 X = -5400604
38
Y = 13055934
38 feet Y = 3919338
05 meter
Z = 4298140
70 Z = 1283959
54
XDOT = -6414
410408 XDOT = -1932
519444
YDOT = -14917
773381 feet/sec YDOT = -4568
674218 meter/sec
ZDOT = 19178
643672 ZDOT = 5836
207540
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21592686
08 X = 6581450
72
Y = -3638817
51 feet Y = -1109111
58 meter
Z = 4189554
81 Z = 1276976
31
XDOT = -1227
632018 XDOT = -374
182239
YDOT = 14680
921863 feet/sec YDOT = 4474
744984 meter/sec
ZDOT = 19139
963382 ZDOT = 5833
860839
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
36155294
00016717 00000-0 10270-3 0 9088
2 25544 51
6477 135
1819 0016390 255
3489 104
5846 15
51414086 40103
Satellite: ISS
Catalog Number: 25544
Epoch time: 12311
36155294 = yrday
fracday
Element set: 908
Inclination: 51
6477 deg
RA of node: 135
1819 deg
Eccentricity:
0016390
Arg of perigee: 255
3489 deg
Mean anomaly: 104
5846 deg
Mean motion: 15
51414086 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4010
Checksum: 305
Coasting Arc #10 (Orbit 4024)
---------------------------------------
Vector Time (GMT): 2012/312/07:11:27
081
Vector Time (MET): N/A
Weight (LBS) : 891465
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5237181
07 A = 6795430
08 meter
Y = -3783857
66 meter E =
0014536
Z = -2078265
53 I = 51
93027
XDOT = 1454
158566 Wp = 235
52749
YDOT = 5077
066245 meter/sec RA = 129
55968 deg
ZDOT = -5559
661208 TA = 327
36191
MA = 327
45166
Ha = 225
353 n
mi
Hp = 219
242
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17182352
58 X = 5289199
61
Y = -12414231
18 feet Y = -3725001
43 meter
Z = -6818456
48 Z = -2052696
72
XDOT = 4770
861438 XDOT = 1424
285651
YDOT = 16657
041487 feet/sec YDOT = 5093
160383 meter/sec
ZDOT = -18240
358295 ZDOT = -5552
669560
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20926104
03 X = -6378276
51
Y = 3589308
30 feet Y = 1094021
17 meter
Z = -6712135
33 Z = -2045858
85
XDOT = 3189
829528 XDOT = 972
260040
YDOT = -15582
001688 feet/sec YDOT = -4749
394115 meter/sec
ZDOT = -18211
888679 ZDOT = -5550
983669
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
32775630
00016717 00000-0 10270-3 0 9098
2 25544 51
6482 130
3856 0016564 258
6660 101
2631 15
51426007 40255
Satellite: ISS
Catalog Number: 25544
Epoch time: 12312
32775630 = yrday
fracday
Element set: 909
Inclination: 51
6482 deg
RA of node: 130
3856 deg
Eccentricity:
0016564
Arg of perigee: 258
6660 deg
Mean anomaly: 101
2631 deg
Mean motion: 15
51426007 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4025
Checksum: 287
Coasting Arc #11 (Orbit 4040)
---------------------------------------
Vector Time (GMT): 2012/313/07:11:27
081
Vector Time (MET): N/A
Weight (LBS) : 891465
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5099599
13 A = 6793753
89 meter
Y = 3483853
10 meter E =
0003133
Z = 2832653
54 I = 51
94355
XDOT = -994
084731 Wp = 277
48592
YDOT = -5611
260156 meter/sec RA = 124
61761 deg
ZDOT = 5116
831603 TA = 114
48279
MA = 114
45011
Ha = 224
991 n
mi
Hp = 219
255
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16730968
26 X = -5151937
90
Y = 11429964
23 feet Y = 3426533
66 meter
Z = 9293482
76 Z = 2807752
25
XDOT = -3261
432843 XDOT = -956
121385
YDOT = -18409
646182 feet/sec YDOT = -5622
164169 meter/sec
ZDOT = 16787
505258 ZDOT = 5112
094737
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20049235
54 X = 6111006
99
Y = -3242104
00 feet Y = -988193
30 meter
Z = 9189946
62 Z = 2801095
73
XDOT = -4987
648063 XDOT = -1520
235129
YDOT = 16638
200119 feet/sec YDOT = 5071
323396 meter/sec
ZDOT = 16768
435666 ZDOT = 5111
019191
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
35835430
00016717 00000-0 10270-3 0 9109
2 25544 51
6480 125
2680 0016407 263
3399 96
5885 15
51469666 40412
Satellite: ISS
Catalog Number: 25544
Epoch time: 12313
35835430 = yrday
fracday
Element set: 910
Inclination: 51
6480 deg
RA of node: 125
2680 deg
Eccentricity:
0016407
Arg of perigee: 263
3399 deg
Mean anomaly: 96
5885 deg
Mean motion: 15
51469666 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4041
Checksum: 315
Coasting Arc #12 (Orbit 4055)
---------------------------------------
Vector Time (GMT): 2012/314/07:11:27
081
Vector Time (MET): N/A
Weight (LBS) : 891465
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4918785
40 A = 6791899
08 meter
Y = -3100876
53 meter E =
0011663
Z = -3499267
25 I = 51
95397
XDOT = 613
041565 Wp = 266
63849
YDOT = 6132
734231 meter/sec RA = 119
67541 deg
ZDOT = -4560
385423 TA = 314
26278
MA = 314
35844
Ha = 225
035 n
mi
Hp = 219
058
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16137747
38 X = 4970093
45
Y = -10173479
41 feet Y = -3045584
88 meter
Z = -11480535
61 Z = -3475246
78
XDOT = 2011
291225 XDOT = 566
572240
YDOT = 20120
519130 feet/sec YDOT = 6139
329601 meter/sec
ZDOT = -14961
894434 ZDOT = -4557
520407
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18948567
39 X = -5775523
34
Y = 2676046
39 feet Y = 815658
94 meter
Z = -11380678
43 Z = -3468830
79
XDOT = 6483
962771 XDOT = 1976
311853
YDOT = -17844
998819 feet/sec YDOT = -5439
155640 meter/sec
ZDOT = -14950
640734 ZDOT = -4556
955296
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
32452029
00016717 00000-0 10270-3 0 9117
2 25544 51
6479 120
4713 0016656 266
8531 93
0715 15
51497692 40566
Satellite: ISS
Catalog Number: 25544
Epoch time: 12314
32452029 = yrday
fracday
Element set: 911
Inclination: 51
6479 deg
RA of node: 120
4713 deg
Eccentricity:
0016656
Arg of perigee: 266
8531 deg
Mean anomaly: 93
0715 deg
Mean motion: 15
51497692 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4056
Checksum: 307
Coasting Arc #13 (Orbit 4071)
---------------------------------------
Vector Time (GMT): 2012/315/07:11:27
081
Vector Time (MET): N/A
Weight (LBS) : 891465
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4740603
91 A = 6789880
95 meter
Y = 2605560
42 meter E =
0006401
Z = 4110357
73 I = 51
96148
XDOT = -284
412165 Wp = 251
93499
YDOT = -6605
782570 meter/sec RA = 114
73008 deg
ZDOT = 3862
394701 TA = 158
25456
MA = 158
22738
Ha = 224
822 n
mi
Hp = 219
170
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15553162
43 X = -4789355
15
Y = 8548426
58 feet Y = 2552275
64 meter
Z = 13485425
63 Z = 4087209
01
XDOT = -933
110779 XDOT = -229
286866
YDOT = -21672
514993 feet/sec YDOT = -6608
654635 meter/sec
ZDOT = 12671
898624 ZDOT = 3861
147227
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17735959
80 X = 5405920
55
Y = -1731359
87 feet Y = -527718
49 meter
Z = 13389222
76 Z = 4081035
10
XDOT = -7696
906729 XDOT = -2346
017171
YDOT = 19038
117675 feet/sec YDOT = 5802
818267 meter/sec
ZDOT = 12667
406532 ZDOT = 3861
025511
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
35507936
00016717 00000-0 10270-3 0 9120
2 25544 51
6476 115
3532 0016452 271
3052 88
6215 15
51524019 40725
Satellite: ISS
Catalog Number: 25544
Epoch time: 12315
35507936 = yrday
fracday
Element set: 912
Inclination: 51
6476 deg
RA of node: 115
3532 deg
Eccentricity:
0016452
Arg of perigee: 271
3052 deg
Mean anomaly: 88
6215 deg
Mean motion: 15
51524019 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4072
Checksum: 289
Coasting Arc #14 (Orbit 4086)
---------------------------------------
Vector Time (GMT): 2012/316/07:11:27
081
Vector Time (MET): N/A
Weight (LBS) : 891465
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4555094
01 A = 6787924
21 meter
Y = -2038267
55 meter E =
0008752
Z = -4597584
53 I = 51
96656
XDOT = 29
966941 Wp = 303
88777
YDOT = 7022
271787 meter/sec RA = 109
78365 deg
ZDOT = -3074
588149 TA = 295
45638
MA = 295
54691
Ha = 224
972 n
mi
Hp = 218
917
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14944534
17 X = 4599882
44
Y = -6687229
49 feet Y = -1987079
38 meter
Z = -15083938
75 Z = -4575346
62
XDOT = 98
316735 XDOT = -33
623733
YDOT = 23038
949432 feet/sec YDOT = 7022
251229 meter/sec
ZDOT = -10087
231461 ZDOT = -3074
597287
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16448335
84 X = -5013452
76
Y = 537305
03 feet Y = 163770
57 meter
Z = -14991560
94 Z = -4569427
77
XDOT = 8561
402781 XDOT = 2609
515568
YDOT = -20205
217439 feet/sec YDOT = -6158
550276 meter/sec
ZDOT = -10088
004256 ZDOT = -3074
823697
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
32120740
00016717 00000-0 10270-3 0 9133
2 25544 51
6469 110
5556 0016694 274
9783 84
9462 15
51576378 40872
Satellite: ISS
Catalog Number: 25544
Epoch time: 12316
32120740 = yrday
fracday
Element set: 913
Inclination: 51
6469 deg
RA of node: 110
5556 deg
Eccentricity:
0016694
Arg of perigee: 274
9783 deg
Mean anomaly: 84
9462 deg
Mean motion: 15
51576378 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4087
Checksum: 329
Coasting Arc #15 (Orbit 4102)
---------------------------------------
Vector Time (GMT): 2012/317/07:11:27
081
Vector Time (MET): N/A
Weight (LBS) : 891465
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4400761
60 A = 6786350
40 meter
Y = 1370195
28 meter E =
0011005
Z = 4990741
87 I = 51
97097
XDOT = 181
414771 Wp = 265
63448
YDOT = -7337
341607 meter/sec RA = 104
83460 deg
ZDOT = 2177
732521 TA = 163
21477
MA = 163
17833
Ha = 224
947 n
mi
Hp = 219
103
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14438194
23 X = -4440000
97
Y = 4495391
35 feet Y = 1320763
88 meter
Z = 16373825
04 Z = 4969267
19
XDOT = 595
192819 XDOT = 252
869722
YDOT = -24072
643067 feet/sec YDOT = -7334
913360 meter/sec
ZDOT = 7144
791735 ZDOT = 2178
787511
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15181901
70 X = 4627443
64
Y = 1044713
97 feet Y = 318428
82 meter
Z = 16284673
04 Z = 4963568
34
XDOT = -9112
899938 XDOT = -2777
611901
YDOT = 21149
005966 feet/sec YDOT = 6446
217019 meter/sec
ZDOT = 7149
949993 ZDOT = 2179
304758
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
35172664
00016717 00000-0 10270-3 0 9140
2 25544 51
6471 105
4374 0016524 279
0659 80
8622 15
51581499 41038
Satellite: ISS
Catalog Number: 25544
Epoch time: 12317
35172664 = yrday
fracday
Element set: 914
Inclination: 51
6471 deg
RA of node: 105
4374 deg
Eccentricity:
0016524
Arg of perigee: 279
0659 deg
Mean anomaly: 80
8622 deg
Mean motion: 15
51581499 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4103
Checksum: 312
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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