[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
January 26th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 16145 87 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 119 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 152 ET - UTC (sec) : 66 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
032/21:57:47
723 3
1 4
9 4
9
N/A 0
3 -0
0 219
2
000/00:01:35
445 -3
8 -0
1 205
4
Coasting Arc #1 (Orbit 3529)
---------------------------------------
Vector Time (GMT): 2012/023/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5344289
54 A = 6768887
54 meter
Y = -1323138
67 meter E =
0019612
Z = -3942646
06 I = 51
89662
XDOT = -1435
027862 Wp = 330
27965
YDOT = 6352
917905 meter/sec RA = 131
92989 deg
ZDOT = -4051
978996 TA = 257
44254
MA = 257
66198
Ha = 217
386 n
mi
Hp = 205
095
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17533758
35 X = 5377839
91
Y = -4341006
13 feet Y = -1263187
74 meter
Z = -12935190
47 Z = -3916603
02
XDOT = -4708
096659 XDOT = -1486
277741
YDOT = 20842
906513 feet/sec YDOT = 6336
584195 meter/sec
ZDOT = -13293
894343 ZDOT = -4059
074263
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12891218
62 X = 3929243
43
Y = 12761085
16 feet Y = 3889578
76 meter
Z = -12828380
90 Z = -3910090
50
XDOT = -19265
119406 XDOT = -5872
008395
YDOT = 5984
019049 feet/sec YDOT = 1823
929006 meter/sec
ZDOT = -13323
390692 ZDOT = -4060
969483
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 12023
52356006
00016717 00000-0 10270-3 0 9002
2 25544 51
6423 132
7663 0022117 313
3255 46
6056 15
58933883 35307
Satellite: ISS
Catalog Number: 25544
Epoch time: 12023
52356006 = yrday
fracday
Element set: 900
Inclination: 51
6423 deg
RA of node: 132
7663 deg
Eccentricity:
0022117
Arg of perigee: 313
3255 deg
Mean anomaly: 46
6056 deg
Mean motion: 15
58933883 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3530
Checksum: 283
Coasting Arc #2 (Orbit 3545)
---------------------------------------
Vector Time (GMT): 2012/024/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3742861
64 A = 6763330
03 meter
Y = -1935938
51 meter E =
0019456
Z = 5299369
70 I = 51
89884
XDOT = 4182
609678 Wp = 320
75870
YDOT = -6396
462094 meter/sec RA = 126
90619 deg
ZDOT = 633
336221 TA = 123
31035
MA = 123
12389
Ha = 217
577 n
mi
Hp = 204
820
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12279729
78 X = -3746677
85
Y = -6351504
31 feet Y = -1977814
98 meter
Z = 17386383
53 Z = 5281178
22
XDOT = 13722
472696 XDOT = 4250
748815
YDOT = -20985
768024 feet/sec YDOT = -6349
308609 meter/sec
ZDOT = 2077
874740 ZDOT = 653
819927
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1280951
34 X = -390433
97
Y = -13859111
41 feet Y = -4224257
16 meter
Z = 17311958
23 Z = 5276684
87
XDOT = 24054
282030 XDOT = 7331
745163
YDOT = 412
053903 feet/sec YDOT = 125
594030 meter/sec
ZDOT = 2162
247157 ZDOT = 659
052934
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 12024
54920366
00016717 00000-0 10270-3 0 9012
2 25544 51
6429 127
6154 0022194 317
4661 42
4774 15
59005118 35462
Satellite: ISS
Catalog Number: 25544
Epoch time: 12024
54920366 = yrday
fracday
Element set: 901
Inclination: 51
6429 deg
RA of node: 127
6154 deg
Eccentricity:
0022194
Arg of perigee: 317
4661 deg
Mean anomaly: 42
4774 deg
Mean motion: 15
59005118 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3546
Checksum: 298
Coasting Arc #3 (Orbit 3560)
---------------------------------------
Vector Time (GMT): 2012/025/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1296120
45 A = 6766010
85 meter
Y = 4763717
76 meter E =
0014352
Z = -4616403
23 I = 51
92542
XDOT = -5522
632721 Wp = 343
67599
YDOT = 4411
237085 meter/sec RA = 121
87809 deg
ZDOT = 3012
622724 TA = 316
14039
MA = 316
25425
Ha = 217
789 n
mi
Hp = 204
545
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4252363
67 X = 1265180
15
Y = 15628995
26 feet Y = 4778038
80 meter
Z = -15145679
90 Z = -4610182
02
XDOT = -18118
873758 XDOT = -5586
183874
YDOT = 14472
562616 feet/sec YDOT = 4349
124256 meter/sec
ZDOT = 9883
932821 ZDOT = 2985
640367
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10652922
21 X = -3247010
69
Y = 12232148
27 feet Y = 3728358
79 meter
Z = -15120499
54 Z = -4608728
26
XDOT = -21199
440883 XDOT = -6461
589581
YDOT = -6427
155063 feet/sec YDOT = -1958
996863 meter/sec
ZDOT = 9773
049577 ZDOT = 2978
825511
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 12025
51072700
00016717 00000-0 10270-3 0 9021
2 25544 51
6426 122
7883 0022131 321
3787 38
5784 15
59034588 35615
Satellite: ISS
Catalog Number: 25544
Epoch time: 12025
51072700 = yrday
fracday
Element set: 902
Inclination: 51
6426 deg
RA of node: 122
7883 deg
Eccentricity:
0022131
Arg of perigee: 321
3787 deg
Mean anomaly: 38
5784 deg
Mean motion: 15
59034588 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3561
Checksum: 300
Coasting Arc #4 (Orbit 3576)
---------------------------------------
Vector Time (GMT): 2012/026/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1300308
89 A = 6773109
10 meter
Y = -6296500
39 meter E =
0013596
Z = 2156432
21 I = 51
96368
XDOT = 5252
031393 Wp = 2
43449
YDOT = -810
716200 meter/sec RA = 116
88013 deg
ZDOT = -5519
607613 TA = 153
75332
MA = 153
68436
Ha = 217
992 n
mi
Hp = 204
402
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4266105
29 X = 1360145
75
Y = -20657809
69 feet Y = -6281624
95 meter
Z = 7074908
81 Z = 2162894
32
XDOT = 17231
074123 XDOT = 5287
519048
YDOT = -2659
830052 feet/sec YDOT = -751
786391 meter/sec
ZDOT = -18108
948860 ZDOT = -5494
007848
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19430789
89 X = 5922504
76
Y = -8185820
44 feet Y = -2495038
07 meter
Z = 7101819
36 Z = 2164634
54
XDOT = 11395
188039 XDOT = 3473
253314
YDOT = 11387
974139 feet/sec YDOT = 3471
054518 meter/sec
ZDOT = -18003
966162 ZDOT = -5487
608886
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 12026
53633029
00016717 00000-0 10270-3 0 9032
2 25544 51
6419 117
6379 0022164 325
4544 34
5170 15
59033213 35778
Satellite: ISS
Catalog Number: 25544
Epoch time: 12026
53633029 = yrday
fracday
Element set: 903
Inclination: 51
6419 deg
RA of node: 117
6379 deg
Eccentricity:
0022164
Arg of perigee: 325
4544 deg
Mean anomaly: 34
5170 deg
Mean motion: 15
59033213 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3577
Checksum: 294
Coasting Arc #5 (Orbit 3592)
---------------------------------------
Vector Time (GMT): 2012/027/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3297788
15 A = 6774507
03 meter
Y = 5783611
68 meter E =
0026584
Z = 1153234
75 I = 51
98160
XDOT = -3670
676426 Wp =
54659
YDOT = -3267
611447 meter/sec RA = 111
90859 deg
ZDOT = 5915
576227 TA = 11
96544
MA = 11
90241
Ha = 218
288 n
mi
Hp = 204
086
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10819514
91 X = -3367818
60
Y = 18975103
95 feet Y = 5746342
25 meter
Z = 3783578
59 Z = 1137044
34
XDOT = -12042
901660 XDOT = -3662
600515
YDOT = -10720
509997 feet/sec YDOT = -3308
613942 meter/sec
ZDOT = 19408
058486 ZDOT = 5897
764265
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21748606
43 X = -6628975
24
Y = 2148326
54 feet Y = 654809
93 meter
Z = 3716820
07 Z = 1132886
76
XDOT = 1854
435664 XDOT = 565
231990
YDOT = -14535
431614 feet/sec YDOT = -4430
399556 meter/sec
ZDOT = 19335
270647 ZDOT = 5893
390493
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 12027
56191144
00016717 00000-0 10270-3 0 9044
2 25544 51
6423 112
4865 0022302 329
5890 30
3970 15
59056295 35934
Satellite: ISS
Catalog Number: 25544
Epoch time: 12027
56191144 = yrday
fracday
Element set: 904
Inclination: 51
6423 deg
RA of node: 112
4865 deg
Eccentricity:
0022302
Arg of perigee: 329
5890 deg
Mean anomaly: 30
3970 deg
Mean motion: 15
59056295 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3593
Checksum: 302
Coasting Arc #6 (Orbit 3607)
---------------------------------------
Vector Time (GMT): 2012/028/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4301539
05 A = 6768200
38 meter
Y = -3369434
64 meter E =
0022190
Z = -4007537
41 I = 51
97002
XDOT = 1299
533557 Wp = 350
88714
YDOT = 6421
042552 meter/sec RA = 106
92381 deg
ZDOT = -3979
419810 TA = 237
77461
MA = 237
98991
Ha = 218
424 n
mi
Hp = 203
970
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14112660
91 X = 4358364
44
Y = -11054575
59 feet Y = -3321014
53 meter
Z = -13148088
63 Z = -3986502
98
XDOT = 4263
561538 XDOT = 1246
966407
YDOT = 21066
412572 feet/sec YDOT = 6435
280745 meter/sec
ZDOT = -13055
839273 ZDOT = -3973
234634
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17317698
66 X = 5278434
55
Y = 4871771
78 feet Y = 1484916
04 meter
Z = -13061631
86 Z = -3981185
39
XDOT = -14031
702552 XDOT = -4276
862938
YDOT = 14725
822854 feet/sec YDOT = 4488
430806 meter/sec
ZDOT = -13030
931361 ZDOT = -3971
827879
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 12028
52337374
00016717 00000-0 10270-3 0 9059
2 25544 51
6411 107
6583 0022278 333
0682 26
9315 15
59092021 36083
Satellite: ISS
Catalog Number: 25544
Epoch time: 12028
52337374 = yrday
fracday
Element set: 905
Inclination: 51
6411 deg
RA of node: 107
6583 deg
Eccentricity:
0022278
Arg of perigee: 333
0682 deg
Mean anomaly: 26
9315 deg
Mean motion: 15
59092021 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3608
Checksum: 296
Coasting Arc #7 (Orbit 3623)
---------------------------------------
Vector Time (GMT): 2012/029/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4174169
49 A = 6762819
33 meter
Y = -351950
98 meter E =
0020582
Z = 5313303
28 I = 51
96110
XDOT = 1215
278253 Wp = 342
29956
YDOT = -7561
982717 meter/sec RA = 101
90175 deg
ZDOT = 473
409263 TA = 103
32260
MA = 103
09301
Ha = 218
622 n
mi
Hp = 203
599
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13694781
78 X = -4195734
15
Y = -1154694
81 feet Y = -398749
63 meter
Z = 17432097
38 Z = 5292973
25
XDOT = 3987
133377 XDOT = 1297
447850
YDOT = -24809
654582 feet/sec YDOT = -7547
933287 meter/sec
ZDOT = 1553
179998 ZDOT = 479
512613
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7456396
94 X = -2272709
79
Y = -11669628
46 feet Y = -3556902
75 meter
Z = 17348783
92 Z = 5287909
34
XDOT = 21283
238716 XDOT = 6487
131161
YDOT = -11348
002545 feet/sec YDOT = -3458
871176 meter/sec
ZDOT = 1578
735742 ZDOT = 481
198654
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 12029
54891151
00016717 00000-0 10270-3 0 9061
2 25544 51
6416 102
5062 0022365 336
9157 23
0992 15
59156916 36241
Satellite: ISS
Catalog Number: 25544
Epoch time: 12029
54891151 = yrday
fracday
Element set: 906
Inclination: 51
6416 deg
RA of node: 102
5062 deg
Eccentricity:
0022365
Arg of perigee: 336
9157 deg
Mean anomaly: 23
0992 deg
Mean motion: 15
59156916 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3624
Checksum: 306
Coasting Arc #8 (Orbit 3638)
---------------------------------------
Vector Time (GMT): 2012/030/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3085811
32 A = 6765976
39 meter
Y = 3963726
64 meter E =
0017893
Z = -4524791
93 I = 51
97634
XDOT = -3264
626301 Wp = 6
10104
YDOT = 6173
167154 meter/sec RA = 96
87610 deg
ZDOT = 3199
787239 TA = 295
73071
MA = 295
91532
Ha = 218
831 n
mi
Hp = 203
244
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10124052
90 X = 3063238
96
Y = 13004352
48 feet Y = 3998107
88 meter
Z = -14845117
87 Z = -4509856
19
XDOT = -10710
716212 XDOT = -3348
956919
YDOT = 20253
173078 feet/sec YDOT = 6136
188570 meter/sec
ZDOT = 10497
989629 ZDOT = 3183
723192
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3862891
50 X = -1177409
33
Y = 16077727
50 feet Y = 4900491
34 meter
Z = -14784177
46 Z = -4506217
29
XDOT = -21396
924852 XDOT = -6521
782695
YDOT = 4395
495310 feet/sec YDOT = 1339
746971 meter/sec
ZDOT = 10431
687857 ZDOT = 3179
578459
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 12030
51033572
00016717 00000-0 10270-3 0 9076
2 25544 51
6407 97
6776 0022390 341
1871 18
8455 15
59185666 36392
Satellite: ISS
Catalog Number: 25544
Epoch time: 12030
51033572 = yrday
fracday
Element set: 907
Inclination: 51
6407 deg
RA of node: 97
6776 deg
Eccentricity:
0022390
Arg of perigee: 341
1871 deg
Mean anomaly: 18
8455 deg
Mean motion: 15
59185666 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3639
Checksum: 322
Coasting Arc #9 (Orbit 3654)
---------------------------------------
Vector Time (GMT): 2012/031/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1292482
53 A = 6772968
97 meter
Y = -6373948
24 meter E =
0017824
Z = 1921548
87 I = 52
00337
XDOT = 4487
500409 Wp = 23
22560
YDOT = -2617
778611 meter/sec RA = 91
88185 deg
ZDOT = -5631
295174 TA = 135
70144
MA = 135
55866
Ha = 218
937 n
mi
Hp = 202
931
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4240428
26 X = -1230446
05
Y = -20911903
66 feet Y = -6388054
73 meter
Z = 6304294
19 Z = 1915420
72
XDOT = 14722
770371 XDOT = 4543
794662
YDOT = -8588
512502 feet/sec YDOT = -2567
281784 meter/sec
ZDOT = -18475
377867 ZDOT = -5609
358646
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13464433
95 X = 4103959
47
Y = -16562250
83 feet Y = -5048174
05 meter
Z = 6279644
73 Z = 1914035
71
XDOT = 14837
969234 XDOT = 4522
613022
YDOT = 5049
732140 feet/sec YDOT = 1539
158356 meter/sec
ZDOT = -18385
251733 ZDOT = -5603
824728
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 12031
53583216
00016717 00000-0 10270-3 0 9085
2 25544 51
6413 92
5257 0022597 345
0717 14
9769 15
59231957 36556
Satellite: ISS
Catalog Number: 25544
Epoch time: 12031
53583216 = yrday
fracday
Element set: 908
Inclination: 51
6413 deg
RA of node: 92
5257 deg
Eccentricity:
0022597
Arg of perigee: 345
0717 deg
Mean anomaly: 14
9769 deg
Mean motion: 15
59231957 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3655
Checksum: 325
Coasting Arc #10 (Orbit 3670)
---------------------------------------
Vector Time (GMT): 2012/032/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -772866
82 A = 6773787
72 meter
Y = 6552751
26 meter E =
0030040
Z = 1439816
62 I = 52
00530
XDOT = -4665
298056 Wp = 15
30881
YDOT = -1832
725414 meter/sec RA = 86
91240 deg
ZDOT = 5837
403903 TA =
38711
MA =
38479
Ha = 219
246 n
mi
Hp = 202
651
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2535652
30 X = -853077
77
Y = 21498527
75 feet Y = 6543660
06 meter
Z = 4723807
81 Z = 1435867
45
XDOT = -15306
095984 XDOT = -4672
813861
YDOT = -6012
878655 feet/sec YDOT = -1884
937817 meter/sec
ZDOT = 19151
587607 ZDOT = 5814
722071
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18052367
91 X = -5502361
74
Y = 11953477
85 feet Y = 3643420
05 meter
Z = 4707118
89 Z = 1434729
84
XDOT = -4521
541518 XDOT = -1378
165855
YDOT = -14332
644232 feet/sec YDOT = -4368
589962 meter/sec
ZDOT = 19058
735167 ZDOT = 5809
102479
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 12032
56130979
00016717 00000-0 10270-3 0 9094
2 25544 51
6410 87
3739 0022630 349
4886 10
5793 15
59190959 36716
Satellite: ISS
Catalog Number: 25544
Epoch time: 12032
56130979 = yrday
fracday
Element set: 909
Inclination: 51
6410 deg
RA of node: 87
3739 deg
Eccentricity:
0022630
Arg of perigee: 349
4886 deg
Mean anomaly: 10
5793 deg
Mean motion: 15
59190959 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3671
Checksum: 334
Coasting Arc #11 (Orbit 3676)
---------------------------------------
Vector Time (GMT): 2012/032/21:58:35
445
Vector Time (MET): N/A
Weight (LBS) : 884651
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 163224
57 A = 6776766
17 meter
Y = -6710747
52 meter E =
0010986
Z = -982211
73 I = 52
00743
XDOT = 4743
435201 Wp = 10
03672
YDOT = 984
086250 meter/sec RA = 84
83078 deg
ZDOT = -5934
729932 TA = 180
54913
MA = 180
55034
Ha = 219
239 n
mi
Hp = 205
402
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 535513
69 X = 243024
66
Y = -22016888
20 feet Y = -6708476
03 meter
Z = -3222479
44 Z = -981225
17
XDOT = 15562
451448 XDOT = 4760
907613
YDOT = 3228
629428 feet/sec YDOT = 1037
228129 meter/sec
ZDOT = -19470
898726 ZDOT = -5911
644368
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21757355
65 X = -6631642
00
Y = 3417159
60 feet Y = 1041550
25 meter
Z = -3217920
13 Z = -980822
06
XDOT = 601
492892 XDOT = 183
335033
YDOT = -14418
544738 feet/sec YDOT = -4394
772436 meter/sec
ZDOT = -19376
325108 ZDOT = -5905
903893
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 12032
94587379
00016717 00000-0 10270-3 0 9108
2 25544 51
6423 85
4430 0018957 347
2833 12
7841 15
58314400 36774
Satellite: ISS
Catalog Number: 25544
Epoch time: 12032
94587379 = yrday
fracday
Element set: 910
Inclination: 51
6423 deg
RA of node: 85
4430 deg
Eccentricity:
0018957
Arg of perigee: 347
2833 deg
Mean anomaly: 12
7841 deg
Mean motion: 15
58314400 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3677
Checksum: 316
Coasting Arc #12 (Orbit 3692)
---------------------------------------
Vector Time (GMT): 2012/033/21:58:35
445
Vector Time (MET): N/A
Weight (LBS) : 884651
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2017776
55 A = 6771171
88 meter
Y = 5264279
56 meter E =
0019742
Z = 3727309
83 I = 51
98548
XDOT = -4277
250900 Wp = 26
25216
YDOT = -4697
453538 meter/sec RA = 79
85338 deg
ZDOT = 4327
545730 TA = 18
17523
MA = 18
10477
Ha = 219
486 n
mi
Hp = 204
982
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6620001
80 X = -2094598
96
Y = 17271258
41 feet Y = 5241285
87 meter
Z = 12228706
80 Z = 3717321
32
XDOT = -14032
975394 XDOT = -4245
427050
YDOT = -15411
592971 feet/sec YDOT = -4745
106613 meter/sec
ZDOT = 14197
984679 ZDOT = 4306
844487
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18251879
68 X = 5563172
93
Y = 3162224
86 feet Y = 963846
14 meter
Z = 12187341
09 Z = 3714701
56
XDOT = -12098
560412 XDOT = -3687
641214
YDOT = 15545
846820 feet/sec YDOT = 4738
374111 meter/sec
ZDOT = 14113
473466 ZDOT = 4301
786713
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 12033
97191984
00016717 00000-0 10270-3 0 9116
2 25544 51
6425 80
2949 0019093 351
5288 8
5542 15
58353055 36936
Satellite: ISS
Catalog Number: 25544
Epoch time: 12033
97191984 = yrday
fracday
Element set: 911
Inclination: 51
6425 deg
RA of node: 80
2949 deg
Eccentricity:
0019093
Arg of perigee: 351
5288 deg
Mean anomaly: 8
5542 deg
Mean motion: 15
58353055 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3693
Checksum: 326
Coasting Arc #13 (Orbit 3707)
---------------------------------------
Vector Time (GMT): 2012/034/21:58:35
445
Vector Time (MET): N/A
Weight (LBS) : 884651
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3574035
72 A = 6765405
96 meter
Y = -2427664
98 meter E =
0024614
Z = -5220417
95 I = 51
96066
XDOT = 2899
825171 Wp = 29
57564
YDOT = 6983
509282 meter/sec RA = 74
84471 deg
ZDOT = -1243
916796 TA = 228
42478
MA = 228
63604
Ha = 219
508 n
mi
Hp = 204
752
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11725838
97 X = 3626275
85
Y = -7964780
11 feet Y = -2387405
62 meter
Z = -17127355
48 Z = -5202928
99
XDOT = 9513
862109 XDOT = 2827
561201
YDOT = 22911
775858 feet/sec YDOT = 7015
532910 meter/sec
ZDOT = -4081
091849 ZDOT = -1230
005099
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10310033
13 X = -3142498
10
Y = -9853634
81 feet Y = -3003387
89 meter
Z = -17055451
49 Z = -5198501
61
XDOT = 19624
898811 XDOT = 5981
669158
YDOT = -13463
154709 feet/sec YDOT = -4103
569555 meter/sec
ZDOT = -4024
602720 ZDOT = -1226
698909
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 12034
93381777
00016717 00000-0 10270-3 0 9125
2 25544 51
6428 75
4693 0019143 354
8719 5
2237 15
58418207 37085
Satellite: ISS
Catalog Number: 25544
Epoch time: 12034
93381777 = yrday
fracday
Element set: 912
Inclination: 51
6428 deg
RA of node: 75
4693 deg
Eccentricity:
0019143
Arg of perigee: 354
8719 deg
Mean anomaly: 5
2237 deg
Mean motion: 15
58418207 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3708
Checksum: 324
Coasting Arc #14 (Orbit 3723)
---------------------------------------
Vector Time (GMT): 2012/035/21:58:35
445
Vector Time (MET): N/A
Weight (LBS) : 884651
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4510312
67 A = 6766506
16 meter
Y = -1094236
33 meter E =
0023252
Z = 4927636
30 I = 51
95580
XDOT = -764
621161 Wp = 12
49429
YDOT = -7281
506782 meter/sec RA = 69
82123 deg
ZDOT = -2292
656816 TA = 99
93658
MA = 99
67406
Ha = 219
623 n
mi
Hp = 204
410
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14797613
75 X = -4521678
27
Y = -3590014
22 feet Y = -1144737
13 meter
Z = 16166785
75 Z = 4905698
27
XDOT = -2508
599608 XDOT = -672
004115
YDOT = -23889
457946 feet/sec YDOT = -7289
539323 meter/sec
ZDOT = -7521
839949 ZDOT = -2296
146498
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -58986
52 X = -17979
09
Y = 15321614
51 feet Y = 4670028
10 meter
Z = 16076914
69 Z = 4900243
60
XDOT = -21561
576222 XDOT = -6571
968433
YDOT = 7907
626535 feet/sec YDOT = 2410
244568 meter/sec
ZDOT = -7535
565326 ZDOT = -2296
840311
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 12035
95982159
00016717 00000-0 10270-3 0 9130
2 25544 51
6428 70
3208 0019204 358
3640 1
7449 15
58471301 37249
Satellite: ISS
Catalog Number: 25544
Epoch time: 12035
95982159 = yrday
fracday
Element set: 913
Inclination: 51
6428 deg
RA of node: 70
3208 deg
Eccentricity:
0019204
Arg of perigee: 358
3640 deg
Mean anomaly: 1
7449 deg
Mean motion: 15
58471301 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3724
Checksum: 303
Coasting Arc #15 (Orbit 3738)
---------------------------------------
Vector Time (GMT): 2012/036/21:58:35
445
Vector Time (MET): N/A
Weight (LBS) : 884651
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4491992
97 A = 6773072
60 meter
Y = 4089765
06 meter E =
0021535
Z = -2972340
47 I = 51
96594
XDOT = -1738
956576 Wp = 12
82606
YDOT = 5543
545328 meter/sec RA = 64
81994 deg
ZDOT = 5026
944129 TA = 313
25716
MA = 313
43669
Ha = 219
812 n
mi
Hp = 204
142
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14737509
75 X = 4460365
12
Y = 13417864
38 feet Y = 4139820
50 meter
Z = -9751773
20 Z = -2950595
91
XDOT = -5705
238110 XDOT = -1825
235476
YDOT = 18187
484673 feet/sec YDOT = 5523
616757 meter/sec
ZDOT = 16492
598849 ZDOT = 5018
287102
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9343074
30 X = 2847769
05
Y = -17654036
85 feet Y = -5380950
43 meter
Z = -9662934
55 Z = -2945262
45
XDOT = 17771
631796 XDOT = 5416
793371
YDOT = 447
377863 feet/sec YDOT = 136
360772 meter/sec
ZDOT = 16456
650219 ZDOT = 5015
986987
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 12036
92168264
00016717 00000-0 10270-3 0 9142
2 25544 51
6425 65
4944 0019223 1
9436 358
1790 15
58454322 37391
Satellite: ISS
Catalog Number: 25544
Epoch time: 12036
92168264 = yrday
fracday
Element set: 914
Inclination: 51
6425 deg
RA of node: 65
4944 deg
Eccentricity:
0019223
Arg of perigee: 1
9436 deg
Mean anomaly: 358
1790 deg
Mean motion: 15
58454322 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3739
Checksum: 317
Coasting Arc #16 (Orbit 3754)
---------------------------------------
Vector Time (GMT): 2012/037/21:58:35
445
Vector Time (MET): N/A
Weight (LBS) : 884651
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3368494
55 A = 6776748
24 meter
Y = -5888227
10 meter E =
0014722
Z = -57517
33 I = 51
96420
XDOT = 4119
058451 Wp = 44
77441
YDOT = -2306
522953 meter/sec RA = 59
84726 deg
ZDOT = -6033
919071 TA = 135
84237
MA = 135
72475
Ha = 219
788 n
mi
Hp = 203
992
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11051491
31 X = -3302121
47
Y = -19318330
39 feet Y = -5925524
57 meter
Z = -188705
14 Z = -73719
59
XDOT = 13513
971297 XDOT = 4173
854896
YDOT = -7567
332522 feet/sec YDOT = -2260
154772 meter/sec
ZDOT = -19796
322410 ZDOT = -6013
776328
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15718365
07 X = -4790957
67
Y = 15755541
93 feet Y = 4802289
18 meter
Z = -254670
48 Z = -77623
56
XDOT = -9748
501933 XDOT = -2971
343389
YDOT = -10007
691676 feet/sec YDOT = -3050
344423 meter/sec
ZDOT = -19713
532370 ZDOT = -6008
684666
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 12037
94764644
00016717 00000-0 10270-3 0 9150
2 25544 51
6422 60
3459 0019012 6
0203 354
1177 15
58460614 37551
Satellite: ISS
Catalog Number: 25544
Epoch time: 12037
94764644 = yrday
fracday
Element set: 915
Inclination: 51
6422 deg
RA of node: 60
3459 deg
Eccentricity:
0019012
Arg of perigee: 6
0203 deg
Mean anomaly: 354
1177 deg
Mean motion: 15
58460614 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3755
Checksum: 295
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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