[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
May 6th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 20989 63 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 96 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 135 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
125/11:22:02
481 1
7 1
8 1
9
N/A 0
6 -0
3 188
8
000/00:04:00
962 0
5 -0
0 183
9
Coasting Arc #1 (Orbit 3402)
---------------------------------------
Vector Time (GMT): 2011/124/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6324176
06 A = 6728635
27 meter
Y = -1239156
89 meter E =
0014837
Z = 1907072
27 I = 51
80680
XDOT = -691
195107 Wp = 121
54616
YDOT = -5198
782400 meter/sec RA = 24
54884 deg
ZDOT = -5645
748335 TA = 37
28903
MA = 37
18612
Ha = 189
101 n
mi
Hp = 182
810
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20748609
13 X = -6319113
91
Y = -4065475
35 feet Y = -1309849
45 meter
Z = 6256798
78 Z = 1876361
15
XDOT = -2267
700481 XDOT = -605
583480
YDOT = -17056
372703 feet/sec YDOT = -5206
032798 meter/sec
ZDOT = -18522
796375 ZDOT = -5648
898524
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18309686
85 X = -5580792
55
Y = 10645523
44 feet Y = 3244755
54 meter
Z = 6132585
07 Z = 1869211
93
XDOT = -12089
894629 XDOT = -3684
999883
YDOT = -10069
249931 feet/sec YDOT = -3069
107379 meter/sec
ZDOT = -18535
293583 ZDOT = -5649
557484
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 11124
53542669
00016717 00000-0 10270-3 0 9006
2 25544 51
6473 24
9240 0002281 189
7309 170
3811 15
74711620 34034
Satellite: ISS
Catalog Number: 25544
Epoch time: 11124
53542669 = yrday
fracday
Element set: 900
Inclination: 51
6473 deg
RA of node: 24
9240 deg
Eccentricity:
0002281
Arg of perigee: 189
7309 deg
Mean anomaly: 170
3811 deg
Mean motion: 15
74711620 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3403
Checksum: 284
Coasting Arc #2 (Orbit 3417)
---------------------------------------
Vector Time (GMT): 2011/125/11:24:02
962
Vector Time (MET): N/A
Weight (LBS) : 893510
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3487941
99 A = 6720258
49 meter
Y = -2912422
26 meter E =
0011404
Z = -4961481
39 I = 51
74877
XDOT = 6260
617761 Wp = 116
76615
YDOT = 3959
127814 meter/sec RA = 19
54506 deg
ZDOT = 2075
824586 TA = 173
33855
MA = 173
32338
Ha = 188
784 n
mi
Hp = 183
899
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11443379
23 X = 3544352
34
Y = -9555191
13 feet Y = -2873102
23 meter
Z = -16277826
10 Z = -4944399
90
XDOT = 20540
084517 XDOT = 6205
796606
YDOT = 12989
264481 feet/sec YDOT = 4028
831179 meter/sec
ZDOT = 6810
448117 ZDOT = 2106
106200
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4420929
88 X = 1347499
43
Y = -14316359
43 feet Y = -4363626
35 meter
Z = -16208561
32 Z = -4940369
49
XDOT = 23221
325615 XDOT = 7077
860048
YDOT = -683
445345 feet/sec YDOT = -208
314141 meter/sec
ZDOT = 6932
788029 ZDOT = 2113
113791
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 11125
48730114
00016717 00000-0 10270-3 0 9016
2 25544 51
6476 20
0298 0002766 229
7576 130
3346 15
74463078 34182
Satellite: ISS
Catalog Number: 25544
Epoch time: 11125
48730114 = yrday
fracday
Element set: 901
Inclination: 51
6476 deg
RA of node: 20
0298 deg
Eccentricity:
0002766
Arg of perigee: 229
7576 deg
Mean anomaly: 130
3346 deg
Mean motion: 15
74463078 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3418
Checksum: 302
Coasting Arc #3 (Orbit 3433)
---------------------------------------
Vector Time (GMT): 2011/126/11:24:02
962
Vector Time (MET): N/A
Weight (LBS) : 893510
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5638521
51 A = 6728931
30 meter
Y = -3075807
51 meter E =
0007114
Z = -1993544
26 I = 51
74947
XDOT = 3913
670410 Wp = 164
19856
YDOT = -3551
508843 meter/sec RA = 14
44894 deg
ZDOT = -5601
187586 TA = 37
97846
MA = 37
92832
Ha = 188
560 n
mi
Hp = 183
818
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18499086
33 X = -5594023
79
Y = -10091231
99 feet Y = -3138611
92 meter
Z = -6540499
54 Z = -2020828
64
XDOT = 12840
126016 XDOT = 3980
303030
YDOT = -11651
931901 feet/sec YDOT = -3507
370811 meter/sec
ZDOT = -18376
599693 ZDOT = -5582
013194
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20939857
34 X = -6382468
52
Y = 2029077
54 feet Y = 618462
83 meter
Z = -6650752
70 Z = -2027149
42
XDOT = 4309
014687 XDOT = 1313
387677
YDOT = -15389
726808 feet/sec YDOT = -4690
788731 meter/sec
ZDOT = -18298
829837 ZDOT = -5577
483334
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 11126
50281162
00016717 00000-0 10270-3 0 9025
2 25544 51
6477 14
8114 0002981 233
9782 126
1105 15
74511318 34341
Satellite: ISS
Catalog Number: 25544
Epoch time: 11126
50281162 = yrday
fracday
Element set: 902
Inclination: 51
6477 deg
RA of node: 14
8114 deg
Eccentricity:
0002981
Arg of perigee: 233
9782 deg
Mean anomaly: 126
1105 deg
Mean motion: 15
74511318 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3434
Checksum: 280
Coasting Arc #4 (Orbit 3449)
---------------------------------------
Vector Time (GMT): 2011/127/11:24:02
962
Vector Time (MET): N/A
Weight (LBS) : 893510
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3352189
11 A = 6720369
83 meter
Y = 3295184
23 meter E =
0004327
Z = 4800633
62 I = 51
69137
XDOT = -6605
890944 Wp = 58
43486
YDOT = -3077
430605 meter/sec RA = 9
27705 deg
ZDOT = -2496
532298 TA = 55
98003
MA = 55
93894
Ha = 188
352 n
mi
Hp = 183
716
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10997995
78 X = -3412108
11
Y = 10810971
89 feet Y = 3257362
62 meter
Z = 15750110
29 Z = 4784203
29
XDOT = -21672
870552 XDOT = -6558
859775
YDOT = -10096
557103 feet/sec YDOT = -3151
038522 meter/sec
ZDOT = -8190
722763 ZDOT = -2528
509936
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2835696
56 X = -864320
31
Y = 15227838
76 feet Y = 4641445
26 meter
Z = 15683454
66 Z = 4780316
98
XDOT = -22380
328925 XDOT = -6821
524256
YDOT = 4414
399426 feet/sec YDOT = 1345
508945 meter/sec
ZDOT = -8319
967148 ZDOT = -2535
925987
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 11127
51827116
00016717 00000-0 10270-3 0 9033
2 25544 51
6475 9
5927 0002956 242
1017 117
9848 15
74650124 34506
Satellite: ISS
Catalog Number: 25544
Epoch time: 11127
51827116 = yrday
fracday
Element set: 903
Inclination: 51
6475 deg
RA of node: 9
5927 deg
Eccentricity:
0002956
Arg of perigee: 242
1017 deg
Mean anomaly: 117
9848 deg
Mean motion: 15
74650124 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3450
Checksum: 303
Coasting Arc #5 (Orbit 3465)
---------------------------------------
Vector Time (GMT): 2011/128/11:24:02
962
Vector Time (MET): N/A
Weight (LBS) : 893510
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5843653
65 A = 6727717
63 meter
Y = 2316062
45 meter E =
0011004
Z = 2384256
16 I = 51
68614
XDOT = -3788
471199 Wp = 76
11274
YDOT = 3992
476963 meter/sec RA = 4
18046 deg
ZDOT = 5388
915898 TA = 310
75908
MA = 310
85454
Ha = 188
134 n
mi
Hp = 183
679
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19172092
02 X = 5805738
36
Y = 7598630
10 feet Y = 2381197
57 meter
Z = 7822362
72 Z = 2412552
78
XDOT = -12429
367452 XDOT = -3859
012728
YDOT = 13098
677700 feet/sec YDOT = 3949
717171 meter/sec
ZDOT = 17680
170268 ZDOT = 5370
340391
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19923671
57 X = 6072735
10
Y = -5152955
07 feet Y = -1570620
70 meter
Z = 7936750
93 Z = 2419121
68
XDOT = -2763
675901 XDOT = -842
368415
YDOT = 16519
954072 feet/sec YDOT = 5035
282001 meter/sec
ZDOT = 17604
796729 ZDOT = 5365
942043
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 11128
53368418
00016717 00000-0 10270-3 0 9042
2 25544 51
6476 4
3730 0002949 246
6233 113
4621 15
74673487 34667
Satellite: ISS
Catalog Number: 25544
Epoch time: 11128
53368418 = yrday
fracday
Element set: 904
Inclination: 51
6476 deg
RA of node: 4
3730 deg
Eccentricity:
0002949
Arg of perigee: 246
6233 deg
Mean anomaly: 113
4621 deg
Mean motion: 15
74673487 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3466
Checksum: 313
Coasting Arc #6 (Orbit 3480)
---------------------------------------
Vector Time (GMT): 2011/129/11:24:02
962
Vector Time (MET): N/A
Weight (LBS) : 893510
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3275531
89 A = 6720953
55 meter
Y = -3681983
21 meter E =
0008028
Z = -4577931
28 I = 51
63327
XDOT = 6720
305785 Wp = 124
07944
YDOT = 2253
757925 meter/sec RA = 358
99726 deg
ZDOT = 2995
053747 TA = 175
68771
MA = 175
68079
Ha = 187
892 n
mi
Hp = 183
748
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10746495
69 X = 3338699
86
Y = -12079997
42 feet Y = -3645000
77 meter
Z = -15019459
59 Z = -4561865
52
XDOT = 22048
247327 XDOT = 6680
054924
YDOT = 7394
218914 feet/sec YDOT = 2328
683233 meter/sec
ZDOT = 9826
291820 ZDOT = 3027
603375
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1339839
61 X = 408383
11
Y = -16173207
77 feet Y = -4929593
73 meter
Z = -14954258
72 Z = -4558058
06
XDOT = 20811
968663 XDOT = 6343
488049
YDOT = -7485
335070 feet/sec YDOT = -2281
530129 meter/sec
ZDOT = 9957
893972 ZDOT = 3035
166083
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 11129
48558676
00016717 00000-0 10270-3 0 9055
2 25544 51
6476 359
4797 0003175 251
5000 108
5818 15
74770019 34812
Satellite: ISS
Catalog Number: 25544
Epoch time: 11129
48558676 = yrday
fracday
Element set: 905
Inclination: 51
6476 deg
RA of node: 359
4797 deg
Eccentricity:
0003175
Arg of perigee: 251
5000 deg
Mean anomaly: 108
5818 deg
Mean motion: 15
74770019 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3481
Checksum: 331
Coasting Arc #7 (Orbit 3496)
---------------------------------------
Vector Time (GMT): 2011/130/11:24:02
962
Vector Time (MET): N/A
Weight (LBS) : 893510
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5853629
46 A = 6726198
65 meter
Y = -1657322
00 meter E =
0002913
Z = -2865935
32 I = 51
62079
XDOT = 3734
232211 Wp = 161
59246
YDOT = -4434
663020 meter/sec RA = 353
90151 deg
ZDOT = -5066
730685 TA = 51
33874
MA = 51
31268
Ha = 187
668 n
mi
Hp = 183
643
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19204821
07 X = -5820739
72
Y = -5437408
13 feet Y = -1722596
82 meter
Z = -9402674
94 Z = -2894292
44
XDOT = 12251
418014 XDOT = 3808
157188
YDOT = -14549
419358 feet/sec YDOT = -4392
491026 meter/sec
ZDOT = -16623
132169 ZDOT = -5048
410399
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18418171
76 X = -5613858
75
Y = 7549306
29 feet Y = 2301028
56 meter
Z = -9517340
96 Z = -2900885
52
XDOT = 1277
900011 XDOT = 389
503923
YDOT = -17728
380895 feet/sec YDOT = -5403
610497 meter/sec
ZDOT = -16548
772230 ZDOT = -5044
065776
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 11130
50090329
00016717 00000-0 10270-3 0 9067
2 25544 51
6475 354
2601 0003385 255
2428 104
8361 15
74813126 34972
Satellite: ISS
Catalog Number: 25544
Epoch time: 11130
50090329 = yrday
fracday
Element set: 906
Inclination: 51
6475 deg
RA of node: 354
2601 deg
Eccentricity:
0003385
Arg of perigee: 255
2428 deg
Mean anomaly: 104
8361 deg
Mean motion: 15
74813126 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3497
Checksum: 293
Coasting Arc #8 (Orbit 3512)
---------------------------------------
Vector Time (GMT): 2011/131/11:24:02
962
Vector Time (MET): N/A
Weight (LBS) : 893510
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3242495
95 A = 6721683
50 meter
Y = 4079084
34 meter E =
0006730
Z = 4242220
61 I = 51
57642
XDOT = -6644
946527 Wp = 67
89823
YDOT = -1561
455436 meter/sec RA = 348
70764 deg
ZDOT = -3570
592216 TA = 58
40759
MA = 58
34191
Ha = 187
478 n
mi
Hp = 183
536
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10638110
09 X = -3308476
05
Y = 13382822
64 feet Y = 4042455
77 meter
Z = 13918046
61 Z = 4226308
36
XDOT = -21801
005667 XDOT = -6609
646838
YDOT = -5122
885290 feet/sec YDOT = -1635
565807 meter/sec
ZDOT = -11714
541390 ZDOT = -3602
787721
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 128576
33 X = 39190
07
Y = 17147788
75 feet Y = 5226646
01 meter
Z = 13853452
94 Z = 4222532
45
XDOT = -18839
929898 XDOT = -5742
410633
YDOT = 9729
081738 feet/sec YDOT = 2965
424114 meter/sec
ZDOT = -11844
741529 ZDOT = -3610
277218
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 11131
51616917
00016717 00000-0 10270-3 0 9077
2 25544 51
6477 349
0398 0003408 263
2498 96
8278 15
74957944 35134
Satellite: ISS
Catalog Number: 25544
Epoch time: 11131
51616917 = yrday
fracday
Element set: 907
Inclination: 51
6477 deg
RA of node: 349
0398 deg
Eccentricity:
0003408
Arg of perigee: 263
2498 deg
Mean anomaly: 96
8278 deg
Mean motion: 15
74957944 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3513
Checksum: 345
Coasting Arc #9 (Orbit 3528)
---------------------------------------
Vector Time (GMT): 2011/132/11:24:02
962
Vector Time (MET): N/A
Weight (LBS) : 893510
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5705072
75 A = 6724358
32 meter
Y = 1113285
12 meter E =
0009062
Z = 3373196
72 I = 51
55492
XDOT = -3703
326635 Wp = 91
14622
YDOT = 4919
667672 meter/sec RA = 343
60980 deg
ZDOT = 4628
893067 TA = 308
70964
MA = 308
79063
Ha = 187
277 n
mi
Hp = 183
499
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18717430
28 X = 5675813
29
Y = 3652510
25 feet Y = 1176919
07 meter
Z = 11066918
37 Z = 3400841
06
XDOT = -12150
021767 XDOT = -3780
550513
YDOT = 16140
641967 feet/sec YDOT = 4877
822982 meter/sec
ZDOT = 15186
657043 ZDOT = 4610
714691
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16617269
41 X = 5064943
72
Y = -9222921
21 feet Y = -2811146
38 meter
Z = 11178720
48 Z = 3407274
00
XDOT = 365
802021 XDOT = 111
496456
YDOT = 19019
446319 feet/sec YDOT = 5797
127238 meter/sec
ZDOT = 15112
855986 ZDOT = 4606
398504
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 11132
53138905
00016717 00000-0 10270-3 0 9087
2 25544 51
6468 343
8187 0003450 267
8869 92
1900 15
74971833 35292
Satellite: ISS
Catalog Number: 25544
Epoch time: 11132
53138905 = yrday
fracday
Element set: 908
Inclination: 51
6468 deg
RA of node: 343
8187 deg
Eccentricity:
0003450
Arg of perigee: 267
8869 deg
Mean anomaly: 92
1900 deg
Mean motion: 15
74971833 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3529
Checksum: 333
Coasting Arc #10 (Orbit 3543)
---------------------------------------
Vector Time (GMT): 2011/133/11:24:02
962
Vector Time (MET): N/A
Weight (LBS) : 893510
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3217720
22 A = 6722915
76 meter
Y = -4520832
71 meter E =
0002779
Z = -3798749
90 I = 51
52070
XDOT = 6385
105733 Wp = 121
58800
YDOT = 1039
461877 meter/sec RA = 338
40714 deg
ZDOT = 4172
240429 TA = 192
22534
MA = 192
23209
Ha = 187
159 n
mi
Hp = 183
483
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10556824
85 X = 3286487
72
Y = -14832128
31 feet Y = -4484465
65 meter
Z = -12463090
24 Z = -3782951
08
XDOT = 20948
509624 XDOT = 6352
739509
YDOT = 3410
307997 feet/sec YDOT = 1110
682980 meter/sec
ZDOT = 13688
452851 ZDOT = 4203
180994
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1738834
30 X = -529996
69
Y = -18166175
06 feet Y = -5537050
16 meter
Z = -12398941
02 Z = -3779197
22
XDOT = 16641
755466 XDOT = 5072
407066
YDOT = -11019
289501 feet/sec YDOT = -3358
679440 meter/sec
ZDOT = 13813
590078 ZDOT = 4210
382256
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 11133
48311033
00016717 00000-0 10270-3 0 9098
2 25544 51
6459 338
9237 0003610 270
4140 89
6610 15
75069781 35440
Satellite: ISS
Catalog Number: 25544
Epoch time: 11133
48311033 = yrday
fracday
Element set: 909
Inclination: 51
6459 deg
RA of node: 338
9237 deg
Eccentricity:
0003610
Arg of perigee: 270
4140 deg
Mean anomaly: 89
6610 deg
Mean motion: 15
75069781 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3544
Checksum: 302
Coasting Arc #11 (Orbit 3559)
---------------------------------------
Vector Time (GMT): 2011/134/11:24:02
962
Vector Time (MET): N/A
Weight (LBS) : 893510
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5414078
07 A = 6722171
35 meter
Y = -764387
03 meter E =
0003754
Z = -3914712
56 I = 51
48973
XDOT = 3677
413902 Wp = 49
85625
YDOT = -5433
951254 meter/sec RA = 333
30614 deg
ZDOT = -4025
013353 TA = 178
21291
MA = 178
21157
Ha = 187
012 n
mi
Hp = 183
260
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17762723
33 X = -5386110
90
Y = -2507831
46 feet Y = -824774
05 meter
Z = -12843545
13 Z = -3940946
64
XDOT = 12065
006239 XDOT = 3757
457156
YDOT = -17827
924061 feet/sec YDOT = -5392
380520 meter/sec
ZDOT = -13205
424387 ZDOT = -4006
953927
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14806619
74 X = -4513057
70
Y = 9991538
12 feet Y = 3045420
82 meter
Z = -12949648
18 Z = -3947052
77
XDOT = -2207
744900 XDOT = -672
920646
YDOT = -20291
029292 feet/sec YDOT = -6184
705728 meter/sec
ZDOT = -13132
084835 ZDOT = -4002
659458
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 11134
49823288
00016717 00000-0 10270-3 0 9102
2 25544 51
6448 333
7028 0003703 275
1492 84
9249 15
75133836 35601
Satellite: ISS
Catalog Number: 25544
Epoch time: 11134
49823288 = yrday
fracday
Element set: 910
Inclination: 51
6448 deg
RA of node: 333
7028 deg
Eccentricity:
0003703
Arg of perigee: 275
1492 deg
Mean anomaly: 84
9249 deg
Mean motion: 15
75133836 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3560
Checksum: 317
Coasting Arc #12 (Orbit 3575)
---------------------------------------
Vector Time (GMT): 2011/135/11:24:02
962
Vector Time (MET): N/A
Weight (LBS) : 893510
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3187666
36 A = 6724211
03 meter
Y = 4980097
09 meter E =
0009091
Z = 3194129
21 I = 51
47100
XDOT = -5990
171359 Wp = 89
98796
YDOT = -758
327123 meter/sec RA = 328
09882 deg
ZDOT = -4784
012677 TA = 52
59949
MA = 52
51677
Ha = 186
849 n
mi
Hp = 183
256
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10458222
95 X = -3258634
63
Y = 16338901
20 feet Y = 4944053
69 meter
Z = 10479426
54 Z = 3178471
12
XDOT = -19652
793173 XDOT = -5958
006092
YDOT = -2487
949879 feet/sec YDOT = -825
132756 meter/sec
ZDOT = -15695
579648 ZDOT = -4813
035380
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3472291
90 X = 1058354
57
Y = 19120833
77 feet Y = 5828030
13 meter
Z = 10415824
76 Z = 3174743
39
XDOT = -14592
986671 XDOT = -4447
942337
YDOT = 11284
988917 feet/sec YDOT = 3439
664622 meter/sec
ZDOT = -15812
961523 ZDOT = -4819
790672
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 11135
51330423
00016717 00000-0 10270-3 0 9111
2 25544 51
6453 328
4806 0003926 281
2259 78
8463 15
75257445 35768
Satellite: ISS
Catalog Number: 25544
Epoch time: 11135
51330423 = yrday
fracday
Element set: 911
Inclination: 51
6453 deg
RA of node: 328
4806 deg
Eccentricity:
0003926
Arg of perigee: 281
2259 deg
Mean anomaly: 78
8463 deg
Mean motion: 15
75257445 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3576
Checksum: 313
Coasting Arc #13 (Orbit 3591)
---------------------------------------
Vector Time (GMT): 2011/136/11:24:02
962
Vector Time (MET): N/A
Weight (LBS) : 893510
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5022564
56 A = 6719954
05 meter
Y = 625363
56 meter E =
0005278
Z = 4417722
36 I = 51
42994
XDOT = -3612
383044 Wp = 116
65637
YDOT = 5974
771791 meter/sec RA = 322
98816 deg
ZDOT = 3255
866925 TA = 300
59595
MA = 300
64800
Ha = 186
745 n
mi
Hp = 183
175
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16478230
18 X = 4993737
42
Y = 2051717
71 feet Y = 681367
38 meter
Z = 14493839
77 Z = 4442052
48
XDOT = -11851
650407 XDOT = -3694
742319
YDOT = 19602
269654 feet/sec YDOT = 5933
915165 meter/sec
ZDOT = 10681
978100 ZDOT = 3238
118072
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13206852
37 X = 4025448
60
Y = -9922627
24 feet Y = -3024416
78 meter
Z = 14592241
98 Z = 4447715
36
XDOT = 4344
053197 XDOT = 1324
067415
YDOT = 21410
256371 feet/sec YDOT = 6525
846142 meter/sec
ZDOT = 10609
864035 ZDOT = 3233
886558
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 11136
52832935
00016717 00000-0 10270-3 0 9129
2 25544 51
6438 323
2575 0003866 285
0758 74
9978 15
75265952 35924
Satellite: ISS
Catalog Number: 25544
Epoch time: 11136
52832935 = yrday
fracday
Element set: 912
Inclination: 51
6438 deg
RA of node: 323
2575 deg
Eccentricity:
0003866
Arg of perigee: 285
0758 deg
Mean anomaly: 74
9978 deg
Mean motion: 15
75265952 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3592
Checksum: 347
Coasting Arc #14 (Orbit 3606)
---------------------------------------
Vector Time (GMT): 2011/137/11:24:02
962
Vector Time (MET): N/A
Weight (LBS) : 893510
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3096883
30 A = 6725718
34 meter
Y = -5443192
03 meter E =
0004852
Z = -2445145
47 I = 51
42558
XDOT = 5508
958494 Wp = 3
53112
YDOT = 742
142050 meter/sec RA = 317
78118 deg
ZDOT = 5330
566189 TA = 328
74492
MA = 328
77376
Ha = 186
766 n
mi
Hp = 183
039
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10160378
29 X = 3169398
22
Y = -17858241
58 feet Y = -5408155
08 meter
Z = -8022130
80 Z = -2429925
02
XDOT = 18074
010807 XDOT = 5474
354917
YDOT = 2434
849244 feet/sec YDOT = 803
552497 meter/sec
ZDOT = 17488
734215 ZDOT = 5357
245191
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5423833
95 X = -1653184
59
Y = -19842398
84 feet Y = -6047963
17 meter
Z = -7960269
81 Z = -2426290
24
XDOT = 12973
366000 XDOT = 3954
281957
YDOT = -10598
471156 feet/sec YDOT = -3230
414008 meter/sec
ZDOT = 17596
634858 ZDOT = 5363
454305
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 11137
47986660
00016717 00000-0 10270-3 0 9130
2 25544 51
6431 318
3604 0003879 286
8579 73
2159 15
75367790 36072
Satellite: ISS
Catalog Number: 25544
Epoch time: 11137
47986660 = yrday
fracday
Element set: 913
Inclination: 51
6431 deg
RA of node: 318
3604 deg
Eccentricity:
0003879
Arg of perigee: 286
8579 deg
Mean anomaly: 73
2159 deg
Mean motion: 15
75367790 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3607
Checksum: 346
Coasting Arc #15 (Orbit 3622)
---------------------------------------
Vector Time (GMT): 2011/138/11:24:02
962
Vector Time (MET): N/A
Weight (LBS) : 893510
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4587839
97 A = 6717664
45 meter
Y = -749164
11 meter E =
0009703
Z = -4858401
71 I = 51
37700
XDOT = 3479
637871 Wp = 58
82053
YDOT = -6472
059548 meter/sec RA = 312
65786 deg
ZDOT = -2286
282839 TA = 188
82089
MA = 188
83795
Ha = 186
737 n
mi
Hp = 182
688
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15051968
41 X = -4555520
17
Y = -2457887
51 feet Y = -800286
78 meter
Z = -15939638
17 Z = -4880611
31
XDOT = 11416
134747 XDOT = 3562
857548
YDOT = -21233
791169 feet/sec YDOT = -6432
682521 meter/sec
ZDOT = -7500
927949 ZDOT = -2269
177252
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12153788
55 X = -3704474
75
Y = 9056317
66 feet Y = 2760365
62 meter
Z = -16029459
23 Z = -4885779
17
XDOT = -6663
475574 XDOT = -2031
027355
YDOT = -22105
064216 feet/sec YDOT = -6737
623573 meter/sec
ZDOT = -7431
383459 ZDOT = -2265
085678
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 11138
49479197
00016717 00000-0 10270-3 0 9146
2 25544 51
6428 313
1377 0003827 292
4022 67
6737 15
75451668 36232
Satellite: ISS
Catalog Number: 25544
Epoch time: 11138
49479197 = yrday
fracday
Element set: 914
Inclination: 51
6428 deg
RA of node: 313
1377 deg
Eccentricity:
0003827
Arg of perigee: 292
4022 deg
Mean anomaly: 67
6737 deg
Mean motion: 15
75451668 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3623
Checksum: 332
Coasting Arc #16 (Orbit 3637)
---------------------------------------
Vector Time (GMT): 2011/139/11:24:02
962
Vector Time (MET): N/A
Weight (LBS) : 893510
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2960430
19 A = 6726751
56 meter
Y = 5843654
34 meter E =
0009858
Z = 1507866
74 I = 51
38910
XDOT = -5002
405575 Wp = 118
29820
YDOT = -1040
578240 meter/sec RA = 307
45960 deg
ZDOT = -5764
708771 TA = 45
01925
MA = 44
93939
Ha = 186
624 n
mi
Hp = 182
737
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9712697
49 X = -3032880
02
Y = 19172094
30 feet Y = 5810143
72 meter
Z = 4947069
37 Z = 1493309
71
XDOT = -16412
091780 XDOT = -4962
393735
YDOT = -3413
970604 feet/sec YDOT = -1096
293651 meter/sec
ZDOT = -18913
086518 ZDOT = -5788
913582
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7381941
74 X = 2250015
84
Y = 20198882
88 feet Y = 6156619
50 meter
Z = 4887868
06 Z = 1489822
18
XDOT = -12137
974752 XDOT = -3699
654704
YDOT = 9055
614739 feet/sec YDOT = 2760
151372 meter/sec
ZDOT = -19010
970139 ZDOT = -5794
543698
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 11139
50966421
00016717 00000-0 10270-3 0 9151
2 25544 51
6433 307
9140 0004211 297
8654 62
2083 15
75568315 36384
Satellite: ISS
Catalog Number: 25544
Epoch time: 11139
50966421 = yrday
fracday
Element set: 915
Inclination: 51
6433 deg
RA of node: 307
9140 deg
Eccentricity:
0004211
Arg of perigee: 297
8654 deg
Mean anomaly: 62
2083 deg
Mean motion: 15
75568315 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3638
Checksum: 309
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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