[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
October 16th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13454 89 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
291/15:24:10
617 0
1 0
9 0
9
N/A -0
6 -0
1 231
0
000/00:00:17
234 0
7 0
0 217
1
Coasting Arc #1 (Orbit 3670)
---------------------------------------
Vector Time (GMT): 2012/289/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 891886
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2295185
98 A = 6788833
21 meter
Y = 4109811
03 meter E =
0019957
Z = -4899533
05 I = 51
31804
XDOT = -4873
239797 Wp = 133
12583
YDOT = -5439
164368 meter/sec RA = 242
73902 deg
ZDOT = -2298
913059 TA = 114
35654
MA = 114
14807
Ha = 231
337 n
mi
Hp = 216
151
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7530137
74 X = -2317170
72
Y = 13483632
00 feet Y = 4084021
41 meter
Z = -16074583
50 Z = -4910737
06
XDOT = -15988
319543 XDOT = -4800
887842
YDOT = -17845
027453 feet/sec YDOT = -5493
255667 meter/sec
ZDOT = -7542
365680 ZDOT = -2322
411353
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1408240
08 X = 429231
57
Y = -15330512
54 feet Y = -4672740
22 meter
Z = -16121283
64 Z = -4913767
25
XDOT = 20637
598153 XDOT = 6290
339917
YDOT = 9862
328477 feet/sec YDOT = 3006
037720 meter/sec
ZDOT = -7639
013897 ZDOT = -2328
371436
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 12289
52024368
00016717 00000-0 10270-3 0 9009
2 25544 51
6461 243
5500 0017358 169
8956 190
2547 15
50800875 36716
Satellite: ISS
Catalog Number: 25544
Epoch time: 12289
52024368 = yrday
fracday
Element set: 900
Inclination: 51
6461 deg
RA of node: 243
5500 deg
Eccentricity:
0017358
Arg of perigee: 169
8956 deg
Mean anomaly: 190
2547 deg
Mean motion: 15
50800875 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3671
Checksum: 319
Coasting Arc #2 (Orbit 3686)
---------------------------------------
Vector Time (GMT): 2012/290/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 891886
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2426649
73 A = 6787842
99 meter
Y = -3782916
32 meter E =
0021105
Z = 5086725
86 I = 51
33083
XDOT = 5054
952401 Wp = 163
54467
YDOT = 5512
985885 meter/sec RA = 237
75482 deg
ZDOT = 1666
846174 TA = 270
15829
MA = 270
40013
Ha = 231
116 n
mi
Hp = 216
326
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7961449
24 X = 2444059
88
Y = -12411142
77 feet Y = -3755682
29 meter
Z = 16688733
13 Z = 5098557
30
XDOT = 16584
489505 XDOT = 4984
831956
YDOT = 18087
224032 feet/sec YDOT = 5569
121575 meter/sec
ZDOT = 5468
655427 ZDOT = 1691
232852
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1979542
83 X = -603364
66
Y = 14555264
77 feet Y = 4436444
70 meter
Z = 16737999
58 Z = 5101742
27
XDOT = -21516
688185 XDOT = -6558
286559
YDOT = -9411
600577 feet/sec YDOT = -2868
655856 meter/sec
ZDOT = 5568
975820 ZDOT = 1697
423830
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 12290
55127041
00016717 00000-0 10270-3 0 9017
2 25544 51
6468 238
4373 0017350 174
2311 185
9043 15
50862900 36877
Satellite: ISS
Catalog Number: 25544
Epoch time: 12290
55127041 = yrday
fracday
Element set: 901
Inclination: 51
6468 deg
RA of node: 238
4373 deg
Eccentricity:
0017350
Arg of perigee: 174
2311 deg
Mean anomaly: 185
9043 deg
Mean motion: 15
50862900 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3687
Checksum: 298
Coasting Arc #3 (Orbit 3701)
---------------------------------------
Vector Time (GMT): 2012/291/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 891886
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2687996
78 A = 6787212
05 meter
Y = 3390191
97 meter E =
0021494
Z = -5240297
07 I = 51
34589
XDOT = -5179
266241 Wp = 135
97684
YDOT = -5554
193503 meter/sec RA = 232
76764 deg
ZDOT = -954
085003 TA = 124
93946
MA = 124
73737
Ha = 230
967 n
mi
Hp = 216
528
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8818887
06 X = -2700249
97
Y = 11122677
06 feet Y = 3360064
36 meter
Z = -17192575
68 Z = -5253385
50
XDOT = -16992
343311 XDOT = -5112
138298
YDOT = -18222
419630 feet/sec YDOT = -5611
736002 meter/sec
ZDOT = -3130
200142 ZDOT = -979
083003
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3055895
80 X = 931437
04
Y = -13793969
87 feet Y = -4204402
02 meter
Z = -17247007
53 Z = -5256887
90
XDOT = 22172
330403 XDOT = 6758
126307
YDOT = 8882
804862 feet/sec YDOT = 2707
478922 meter/sec
ZDOT = -3233
052550 ZDOT = -985
434417
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 12291
51784284
00016717 00000-0 10270-3 0 9023
2 25544 51
6470 233
6418 0017287 177
4997 182
6243 15
50856054 37028
Satellite: ISS
Catalog Number: 25544
Epoch time: 12291
51784284 = yrday
fracday
Element set: 902
Inclination: 51
6470 deg
RA of node: 233
6418 deg
Eccentricity:
0017287
Arg of perigee: 177
4997 deg
Mean anomaly: 182
6243 deg
Mean motion: 15
50856054 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3702
Checksum: 325
Coasting Arc #4 (Orbit 3703)
---------------------------------------
Vector Time (GMT): 2012/291/15:24:19
234
Vector Time (MET): N/A
Weight (LBS) : 891790
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5242843
22 A = 6796857
63 meter
Y = -3629584
78 meter E =
0013515
Z = -2379012
63 I = 51
38173
XDOT = 1259
443017 Wp = 161
48983
YDOT = -5324
361178 meter/sec RA = 232
03352 deg
ZDOT = 5343
508638 TA = 171
93437
MA = 171
91261
Ha = 230
974 n
mi
Hp = 217
079
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17200929
19 X = -5190309
77
Y = -11908086
55 feet Y = -3687919
90 meter
Z = -7805159
54 Z = -2404355
03
XDOT = 4132
030895 XDOT = 1292
929286
YDOT = -17468
376568 feet/sec YDOT = -5310
089843 meter/sec
ZDOT = 17531
196320 ZDOT = 5349
708680
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15509324
69 X = 4727242
17
Y = -13981911
41 feet Y = -4261686
60 meter
Z = -7909614
83 Z = -2410850
60
XDOT = 15067
984239 XDOT = 4592
721596
YDOT = 6774
195829 feet/sec YDOT = 2064
774889 meter/sec
ZDOT = 17557
323837 ZDOT = 5351
472306
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 12291
64671722
00016717 00000-0 10270-3 0 9030
2 25544 51
6494 233
0035 0016595 178
9985 181
1202 15
50700393 37042
Satellite: ISS
Catalog Number: 25544
Epoch time: 12291
64671722 = yrday
fracday
Element set: 903
Inclination: 51
6494 deg
RA of node: 233
0035 deg
Eccentricity:
0016595
Arg of perigee: 178
9985 deg
Mean anomaly: 181
1202 deg
Mean motion: 15
50700393 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3704
Checksum: 306
Coasting Arc #5 (Orbit 3719)
---------------------------------------
Vector Time (GMT): 2012/292/15:24:19
234
Vector Time (MET): N/A
Weight (LBS) : 891790
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5407293
72 A = 6797897
67 meter
Y = 3654283
97 meter E =
0025265
Z = 1840592
08 I = 51
40408
XDOT = -1469
209195 Wp = 151
78323
YDOT = 5012
431234 meter/sec RA = 227
06020 deg
ZDOT = -5625
571867 TA = 7
89445
MA = 7
85476
Ha = 230
815 n
mi
Hp = 217
367
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17740464
96 X = 5357087
48
Y = 11989120
62 feet Y = 3714471
02 meter
Z = 6038687
93 Z = 1866739
03
XDOT = -4820
240142 XDOT = -1497
821670
YDOT = 16444
984365 feet/sec YDOT = 4995
841508 meter/sec
ZDOT = -18456
600612 ZDOT = -5632
778997
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15461992
26 X = -4712815
24
Y = 14767411
61 feet Y = 4501107
06 meter
Z = 6146479
64 Z = 1873446
99
XDOT = -13999
661062 XDOT = -4267
096692
YDOT = -6950
409325 feet/sec YDOT = -2118
484762 meter/sec
ZDOT = -18486
866280 ZDOT = -5634
796842
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 12292
67782746
00016717 00000-0 10270-3 0 9044
2 25544 51
6491 227
8907 0016690 182
5903 177
5164 15
50679470 37200
Satellite: ISS
Catalog Number: 25544
Epoch time: 12292
67782746 = yrday
fracday
Element set: 904
Inclination: 51
6491 deg
RA of node: 227
8907 deg
Eccentricity:
0016690
Arg of perigee: 182
5903 deg
Mean anomaly: 177
5164 deg
Mean motion: 15
50679470 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3720
Checksum: 338
Coasting Arc #6 (Orbit 3734)
---------------------------------------
Vector Time (GMT): 2012/293/15:24:19
234
Vector Time (MET): N/A
Weight (LBS) : 891790
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5589224
42 A = 6798391
37 meter
Y = -3661496
92 meter E =
0010086
Z = -1290334
23 I = 51
42791
XDOT = 1725
243625 Wp = 160
30287
YDOT = -4676
849031 meter/sec RA = 222
08793 deg
ZDOT = 5802
124399 TA = 185
66169
MA = 185
67310
Ha = 230
569 n
mi
Hp = 217
514
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18337350
47 X = -5541597
12
Y = -12012785
18 feet Y = -3723732
84 meter
Z = -4233380
03 Z = -1317371
18
XDOT = 5660
248112 XDOT = 1749
226975
YDOT = -15343
992884 feet/sec YDOT = -4657
422091 meter/sec
ZDOT = 19035
841204 ZDOT = 5810
564037
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15347099
53 X = 4677795
94
Y = -15622919
31 feet Y = -4761865
80 meter
Z = -4344866
47 Z = -1324315
30
XDOT = 12831
228276 XDOT = 3910
958378
YDOT = 7304
412064 feet/sec YDOT = 2226
384797 meter/sec
ZDOT = 19071
175302 ZDOT = 5812
894232
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 12293
64447328
00016717 00000-0 10270-3 0 9057
2 25544 51
6490 223
0964 0016550 186
7389 173
3542 15
50758402 37352
Satellite: ISS
Catalog Number: 25544
Epoch time: 12293
64447328 = yrday
fracday
Element set: 905
Inclination: 51
6490 deg
RA of node: 223
0964 deg
Eccentricity:
0016550
Arg of perigee: 186
7389 deg
Mean anomaly: 173
3542 deg
Mean motion: 15
50758402 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3735
Checksum: 323
Coasting Arc #7 (Orbit 3750)
---------------------------------------
Vector Time (GMT): 2012/294/15:24:19
234
Vector Time (MET): N/A
Weight (LBS) : 891790
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5695787
10 A = 6799028
32 meter
Y = 3614819
88 meter E =
0025576
Z = 696298
48 I = 51
45242
XDOT = -2055
494462 Wp = 163
11113
YDOT = 4391
088845 meter/sec RA = 217
11861 deg
ZDOT = -5951
140324 TA = 9
34548
MA = 9
29798
Ha = 230
467 n
mi
Hp = 217
772
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18686965
55 X = 5651559
59
Y = 11859645
28 feet Y = 3678266
45 meter
Z = 2284443
85 Z = 723861
25
XDOT = -6743
748235 XDOT = -2075
534059
YDOT = 14406
459465 feet/sec YDOT = 4367
990859 meter/sec
ZDOT = -19524
738595 ZDOT = -5961
174725
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14989520
71 X = -4568805
91
Y = 16267630
82 feet Y = 4958373
88 meter
Z = 2398125
89 Z = 730948
77
XDOT = -11812
378778 XDOT = -3600
413052
YDOT = -7985
580814 feet/sec YDOT = -2434
005032 meter/sec
ZDOT = -19566
644426 ZDOT = -5963
913221
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 12294
67554658
00016717 00000-0 10270-3 0 9067
2 25544 51
6487 217
9831 0016702 190
3575 169
7235 15
50724833 37517
Satellite: ISS
Catalog Number: 25544
Epoch time: 12294
67554658 = yrday
fracday
Element set: 906
Inclination: 51
6487 deg
RA of node: 217
9831 deg
Eccentricity:
0016702
Arg of perigee: 190
3575 deg
Mean anomaly: 169
7235 deg
Mean motion: 15
50724833 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3751
Checksum: 338
Coasting Arc #8 (Orbit 3765)
---------------------------------------
Vector Time (GMT): 2012/295/15:24:19
234
Vector Time (MET): N/A
Weight (LBS) : 891790
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5803110
59 A = 6798946
61 meter
Y = -3551089
73 meter E =
0008635
Z = -102332
79 I = 51
47738
XDOT = 2413
282186 Wp = 151
87074
YDOT = -4110
438159 meter/sec RA = 212
14974 deg
ZDOT = 5984
737648 TA = 207
02777
MA = 207
07276
Ha = 230
143 n
mi
Hp = 217
940
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19039076
74 X = -5762473
14
Y = -11650556
86 feet Y = -3615756
52 meter
Z = -335737
48 Z = -130425
52
XDOT = 7917
592474 XDOT = 2429
993775
YDOT = -13485
689499 feet/sec YDOT = -4083
357701 meter/sec
ZDOT = 19634
966037 ZDOT = 5996
502116
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14559509
28 X = 4437738
43
Y = -16916008
80 feet Y = -5155999
48 meter
Z = -451634
47 Z = -137658
19
XDOT = 10821
937046 XDOT = 3298
526412
YDOT = 8801
849897 feet/sec YDOT = 2682
803849 meter/sec
ZDOT = 19684
004661 ZDOT = 5999
684621
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 12295
64215768
00016717 00000-0 10270-3 0 9072
2 25544 51
6481 213
1881 0016549 194
5062 165
5616 15
50818241 37660
Satellite: ISS
Catalog Number: 25544
Epoch time: 12295
64215768 = yrday
fracday
Element set: 907
Inclination: 51
6481 deg
RA of node: 213
1881 deg
Eccentricity:
0016549
Arg of perigee: 194
5062 deg
Mean anomaly: 165
5616 deg
Mean motion: 15
50818241 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3766
Checksum: 326
Coasting Arc #9 (Orbit 3781)
---------------------------------------
Vector Time (GMT): 2012/296/15:24:19
234
Vector Time (MET): N/A
Weight (LBS) : 891790
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5815619
63 A = 6798990
81 meter
Y = 3451733
68 meter E =
0024204
Z = -520046
54 I = 51
50305
XDOT = -2838
095384 Wp = 175
33707
YDOT = 3887
553750 meter/sec RA = 207
18389 deg
ZDOT = -5978
169317 TA = 10
28493
MA = 10
23550
Ha = 230
063 n
mi
Hp = 218
178
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19080116
91 X = 5779115
69
Y = 11324585
56 feet Y = 3516563
44 meter
Z = -1706189
45 Z = -491883
09
XDOT = -9311
336563 XDOT = -2852
315009
YDOT = 12754
441438 feet/sec YDOT = 3855
736599 meter/sec
ZDOT = -19613
416395 ZDOT = -5991
991516
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13951358
26 X = -4252374
00
Y = 17263828
18 feet Y = 5262014
83 meter
Z = -1589975
12 Z = -484624
42
XDOT = -10040
419330 XDOT = -3060
319812
YDOT = -9911
604149 feet/sec YDOT = -3021
056945 meter/sec
ZDOT = -19670
949927 ZDOT = -5995
705538
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 12296
67319376
00016717 00000-0 10270-3 0 9087
2 25544 51
6479 208
0745 0016693 198
3058 161
7494 15
50780587 37827
Satellite: ISS
Catalog Number: 25544
Epoch time: 12296
67319376 = yrday
fracday
Element set: 908
Inclination: 51
6479 deg
RA of node: 208
0745 deg
Eccentricity:
0016693
Arg of perigee: 198
3058 deg
Mean anomaly: 161
7494 deg
Mean motion: 15
50780587 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3782
Checksum: 358
Coasting Arc #10 (Orbit 3797)
---------------------------------------
Vector Time (GMT): 2012/297/15:24:19
234
Vector Time (MET): N/A
Weight (LBS) : 891790
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5816154
18 A = 6798282
40 meter
Y = -3343574
68 meter E =
0009429
Z = 1127663
35 I = 51
52851
XDOT = 3263
453230 Wp = 147
70117
YDOT = -3692
056654 meter/sec RA = 202
21783 deg
ZDOT = 5854
264277 TA = 224
52230
MA = 224
59810
Ha = 229
701 n
mi
Hp = 218
341
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19081870
66 X = -5783811
34
Y = -10969733
21 feet Y = -3408433
64 meter
Z = 3699682
90 Z = 1099487
23
XDOT = 10706
867551 XDOT = 3276
057047
YDOT = -12113
046765 feet/sec YDOT = -3655
491829 meter/sec
ZDOT = 19206
903795 ZDOT = 5870
148998
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13301982
12 X = 4054444
15
Y = -17560098
43 feet Y = -5352318
00 meter
Z = 3583392
62 Z = 1092218
07
XDOT = 9391
782812 XDOT = 2862
615401
YDOT = 11068
423899 feet/sec YDOT = 3373
655604 meter/sec
ZDOT = 19272
956237 ZDOT = 5874
397061
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 12297
70420782
00016717 00000-0 10270-3 0 9097
2 25544 51
6472 202
9592 0016603 202
5200 157
5224 15
50878287 37987
Satellite: ISS
Catalog Number: 25544
Epoch time: 12297
70420782 = yrday
fracday
Element set: 909
Inclination: 51
6472 deg
RA of node: 202
9592 deg
Eccentricity:
0016603
Arg of perigee: 202
5200 deg
Mean anomaly: 157
5224 deg
Mean motion: 15
50878287 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3798
Checksum: 318
Coasting Arc #11 (Orbit 3812)
---------------------------------------
Vector Time (GMT): 2012/298/15:24:19
234
Vector Time (MET): N/A
Weight (LBS) : 891790
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5708290
83 A = 6797642
15 meter
Y = 3223221
90 meter E =
0021100
Z = -1744535
79 I = 51
55415
XDOT = -3740
223406 Wp = 187
50544
YDOT = 3557
942626 meter/sec RA = 197
25464 deg
ZDOT = -5677
386053 TA = 11
66379
MA = 11
61498
Ha = 229
587 n
mi
Hp = 218
559
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18727988
29 X = 5680298
50
Y = 10574875
00 feet Y = 3286898
92 meter
Z = -5723542
61 Z = -1716873
08
XDOT = -12271
074166 XDOT = -3752
151280
YDOT = 11673
040110 feet/sec YDOT = 3516
049974 meter/sec
ZDOT = -18626
594663 ZDOT = -5695
585361
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12567907
83 X = -3830698
31
Y = 17490205
87 feet Y = 5331014
75 meter
Z = -5609354
52 Z = -1709731
26
XDOT = -8993
174395 XDOT = -2741
119556
YDOT = -12446
636455 feet/sec YDOT = -3793
734792 meter/sec
ZDOT = -18702
216379 ZDOT = -5700
435552
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 12298
67077010
00016717 00000-0 10270-3 0 9108
2 25544 51
6469 198
1649 0016637 206
1903 153
8408 15
50851043 38131
Satellite: ISS
Catalog Number: 25544
Epoch time: 12298
67077010 = yrday
fracday
Element set: 910
Inclination: 51
6469 deg
RA of node: 198
1649 deg
Eccentricity:
0016637
Arg of perigee: 206
1903 deg
Mean anomaly: 153
8408 deg
Mean motion: 15
50851043 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3813
Checksum: 313
Coasting Arc #12 (Orbit 3828)
---------------------------------------
Vector Time (GMT): 2012/299/15:24:19
234
Vector Time (MET): N/A
Weight (LBS) : 891790
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5582661
52 A = 6796413
17 meter
Y = -3108087
34 meter E =
0011330
Z = 2330467
13 I = 51
57966
XDOT = 4186
124434 Wp = 155
17393
YDOT = -3463
129224 meter/sec RA = 192
29076 deg
ZDOT = 5389
606689 TA = 230
76095
MA = 230
86156
Ha = 229
240 n
mi
Hp = 218
715
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18315818
64 X = -5558812
38
Y = -10197136
93 feet Y = -3170382
60 meter
Z = 7645889
54 Z = 2303404
59
XDOT = 13734
004048 XDOT = 4198
356839
YDOT = -11361
972520 feet/sec YDOT = -3416
248510 meter/sec
ZDOT = 17682
436644 ZDOT = 5409
973016
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11851903
84 X = 3612460
29
Y = -17340102
82 feet Y = -5285263
34 meter
Z = 7534165
56 Z = 2296413
66
XDOT = 8786
898816 XDOT = 2678
246759
YDOT = 13753
848676 feet/sec YDOT = 4192
173077 meter/sec
ZDOT = 17767
022635 ZDOT = 5415
388499
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 12299
70174868
00016717 00000-0 10270-3 0 9113
2 25544 51
6464 193
0493 0016666 210
2057 149
8134 15
50931536 38299
Satellite: ISS
Catalog Number: 25544
Epoch time: 12299
70174868 = yrday
fracday
Element set: 911
Inclination: 51
6464 deg
RA of node: 193
0493 deg
Eccentricity:
0016666
Arg of perigee: 210
2057 deg
Mean anomaly: 149
8134 deg
Mean motion: 15
50931536 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3829
Checksum: 326
Coasting Arc #13 (Orbit 3843)
---------------------------------------
Vector Time (GMT): 2012/300/15:24:19
234
Vector Time (MET): N/A
Weight (LBS) : 891790
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5343711
40 A = 6795164
47 meter
Y = 3006964
64 meter E =
0016645
Z = -2903249
51 I = 51
60456
XDOT = -4661
033111 Wp = 198
00698
YDOT = 3426
089640 meter/sec RA = 187
32908 deg
ZDOT = -5038
353640 TA = 15
08748
MA = 15
03789
Ha = 229
068 n
mi
Hp = 218
892
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17531861
55 X = 5323793
34
Y = 9865369
57 feet Y = 3066609
75 meter
Z = -9525096
82 Z = -2877338
14
XDOT = -15292
103382 XDOT = -4674
522276
YDOT = 11240
451574 feet/sec YDOT = 3373
891202 meter/sec
ZDOT = -16530
031628 ZDOT = -5061
030225
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11162700
08 X = -3402390
98
Y = 16796198
64 feet Y = 5119481
35 meter
Z = -9418120
48 Z = -2870643
12
XDOT = -8837
434697 XDOT = -2693
650095
YDOT = -15180
569609 feet/sec YDOT = -4627
037617 meter/sec
ZDOT = -16624
182208 ZDOT = -5067
050737
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 12300
66827691
00016717 00000-0 10270-3 0 9121
2 25544 51
6456 188
2547 0016554 213
6901 146
3199 15
50926921 38449
Satellite: ISS
Catalog Number: 25544
Epoch time: 12300
66827691 = yrday
fracday
Element set: 912
Inclination: 51
6456 deg
RA of node: 188
2547 deg
Eccentricity:
0016554
Arg of perigee: 213
6901 deg
Mean anomaly: 146
3199 deg
Mean motion: 15
50926921 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3844
Checksum: 324
Coasting Arc #14 (Orbit 3859)
---------------------------------------
Vector Time (GMT): 2012/301/15:24:19
234
Vector Time (MET): N/A
Weight (LBS) : 891790
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5089924
38 A = 6793643
38 meter
Y = -2927405
49 meter E =
0013365
Z = 3428793
03 I = 51
62981
XDOT = 5074
250396 Wp = 170
53103
YDOT = -3427
876571 meter/sec RA = 182
36665 deg
ZDOT = 4590
488416 TA = 229
49882
MA = 229
61535
Ha = 228
757 n
mi
Hp = 219
052
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16699226
97 X = -5073467
91
Y = -9604348
71 feet Y = -2984231
92 meter
Z = 11249320
98 Z = 3404106
05
XDOT = 16647
803135 XDOT = 5089
904422
YDOT = -11246
314209 feet/sec YDOT = -3371
045244 meter/sec
ZDOT = 15060
657534 ZDOT = 4615
177754
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10563576
49 X = 3219778
11
Y = -16180274
13 feet Y = -4931747
55 meter
Z = 11147398
76 Z = 3397727
14
XDOT = 9082
479779 XDOT = 2768
339837
YDOT = 16411
518754 feet/sec YDOT = 5002
230916 meter/sec
ZDOT = 15163
147657 ZDOT = 4621
727406
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 12301
69922037
00016717 00000-0 10270-3 0 9136
2 25544 51
6452 183
1391 0016686 217
6561 142
3423 15
50976954 38603
Satellite: ISS
Catalog Number: 25544
Epoch time: 12301
69922037 = yrday
fracday
Element set: 913
Inclination: 51
6452 deg
RA of node: 183
1391 deg
Eccentricity:
0016686
Arg of perigee: 217
6561 deg
Mean anomaly: 142
3423 deg
Mean motion: 15
50976954 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3860
Checksum: 313
Coasting Arc #15 (Orbit 3874)
---------------------------------------
Vector Time (GMT): 2012/302/15:24:19
234
Vector Time (MET): N/A
Weight (LBS) : 891790
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4728345
75 A = 6792054
27 meter
Y = 2887189
81 meter E =
0011710
Z = -3916660
00 I = 51
65428
XDOT = -5490
574339 Wp = 203
38455
YDOT = 3474
469287 meter/sec RA = 177
40549 deg
ZDOT = -4073
534007 TA = 24
01151
MA = 23
95695
Ha = 228
539 n
mi
Hp = 219
171
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15512945
38 X = 4714735
91
Y = 9472407
51 feet Y = 2939988
77 meter
Z = -12849934
40 Z = -3893722
58
XDOT = -18013
695339 XDOT = -5509
229683
YDOT = 11399
177450 feet/sec YDOT = 3412
965676 meter/sec
ZDOT = -13364
612884 ZDOT = -4100
253200
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10103469
54 X = -3079537
52
Y = 15189550
04 feet Y = 4629774
85 meter
Z = -12755244
62 Z = -3887798
56
XDOT = -9545
116018 XDOT = -2909
351362
YDOT = -17647
380373 feet/sec YDOT = -5378
921538 meter/sec
ZDOT = -13475
520424 ZDOT = -4107
338625
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 12302
66571479
00016717 00000-0 10270-3 0 9145
2 25544 51
6444 178
3440 0016493 220
7780 139
2137 15
50994802 38754
Satellite: ISS
Catalog Number: 25544
Epoch time: 12302
66571479 = yrday
fracday
Element set: 914
Inclination: 51
6444 deg
RA of node: 178
3440 deg
Eccentricity:
0016493
Arg of perigee: 220
7780 deg
Mean anomaly: 139
2137 deg
Mean motion: 15
50994802 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3875
Checksum: 323
Coasting Arc #16 (Orbit 3890)
---------------------------------------
Vector Time (GMT): 2012/303/15:24:19
234
Vector Time (MET): N/A
Weight (LBS) : 891790
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4363730
96 A = 6790548
19 meter
Y = -2883059
75 meter E =
0014969
Z = 4342232
71 I = 51
67921
XDOT = 5820
160349 Wp = 189
54252
YDOT = -3547
332915 meter/sec RA = 172
44381 deg
ZDOT = 3481
008537 TA = 224
96517
MA = 225
08648
Ha = 228
244 n
mi
Hp = 219
344
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14316702
64 X = -4352261
83
Y = -9458857
45 feet Y = -2931793
37 meter
Z = 14246170
29 Z = 4321061
32
XDOT = 19095
014267 XDOT = 5842
484373
YDOT = -11638
231350 feet/sec YDOT = -3482
123251 meter/sec
ZDOT = 11420
631683 ZDOT = 3509
337793
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9798727
71 X = 2986652
21
Y = -14174098
08 feet Y = -4320265
09 meter
Z = 14158785
45 Z = 4315597
80
XDOT = 10146
859614 XDOT = 3092
762810
YDOT = 18582
245304 feet/sec YDOT = 5663
868369 meter/sec
ZDOT = 11538
224624 ZDOT = 3516
850865
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
69662312
00016717 00000-0 10270-3 0 9157
2 25544 51
6438 173
2282 0016638 224
8518 135
1289 15
51016190 38917
Satellite: ISS
Catalog Number: 25544
Epoch time: 12303
69662312 = yrday
fracday
Element set: 915
Inclination: 51
6438 deg
RA of node: 173
2282 deg
Eccentricity:
0016638
Arg of perigee: 224
8518 deg
Mean anomaly: 135
1289 deg
Mean motion: 15
51016190 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3891
Checksum: 308
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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