[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
April 25th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 19375 04 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
There are no maneuvers
Coasting Arc #1 (Orbit 3181)
---------------------------------------
Vector Time (GMT): 2011/110/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1643660
34 A = 6729352
59 meter
Y = 5850727
50 meter E =
0006425
Z = -2894421
35 I = 51
98888
XDOT = -4399
224481 Wp = 83
62208
YDOT = 3744
733732 meter/sec RA = 96
16295 deg
ZDOT = 5081
611488 TA = 243
30172
MA = 243
36751
Ha = 191
389 n
mi
Hp = 183
415
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5392586
43 X = 1592174
97
Y = 19195300
21 feet Y = 5868820
09 meter
Z = -9496133
02 Z = -2886561
30
XDOT = -14433
151183 XDOT = -4465
457687
YDOT = 12285
871823 feet/sec YDOT = 3695
168514 meter/sec
ZDOT = 16671
953701 ZDOT = 5060
078988
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13682102
82 X = 4170304
94
Y = 14523755
95 feet Y = 4426840
81 meter
Z = -9464494
51 Z = -2884777
93
XDOT = -6176
140843 XDOT = -1882
487729
YDOT = 16603
730479 feet/sec YDOT = 5060
817050 meter/sec
ZDOT = 16584
725400 ZDOT = 5055
024302
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 11110
50585297
00016717 00000-0 10270-3 0 9002
2 25544 51
6398 96
9730 0002559 119
4553 240
6866 15
73720174 31820
Satellite: ISS
Catalog Number: 25544
Epoch time: 11110
50585297 = yrday
fracday
Element set: 900
Inclination: 51
6398 deg
RA of node: 96
9730 deg
Eccentricity:
0002559
Arg of perigee: 119
4553 deg
Mean anomaly: 240
6866 deg
Mean motion: 15
73720174 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3182
Checksum: 316
Coasting Arc #2 (Orbit 3197)
---------------------------------------
Vector Time (GMT): 2011/111/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3525503
57 A = 6724389
16 meter
Y = -3655260
57 meter E =
0010889
Z = -4417850
27 I = 51
97520
XDOT = 2498
351354 Wp = 80
27158
YDOT = 6455
693871 meter/sec RA = 91
09998 deg
ZDOT = -3352
786565 TA = 156
15559
MA = 156
10511
Ha = 191
252 n
mi
Hp = 183
416
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11566612
75 X = 3587576
64
Y = -11992324
70 feet Y = -3615489
04 meter
Z = -14494259
43 Z = -4400572
60
XDOT = 8196
690793 XDOT = 2442
264216
YDOT = 21180
098003 feet/sec YDOT = 6483
318460 meter/sec
ZDOT = -10999
955921 ZDOT = -3340
785513
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4538866
95 X = 1383446
65
Y = -16094285
82 feet Y = -4905538
32 meter
Z = -14424236
18 Z = -4396507
19
XDOT = 16174
979829 XDOT = 4930
133852
YDOT = 14361
546579 feet/sec YDOT = 4377
399397 meter/sec
ZDOT = -10951
588884 ZDOT = -3338
044292
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 11111
52183552
00016717 00000-0 10270-3 0 9014
2 25544 51
6401 91
7564 0002520 124
7904 235
3497 15
73788471 31982
Satellite: ISS
Catalog Number: 25544
Epoch time: 11111
52183552 = yrday
fracday
Element set: 901
Inclination: 51
6401 deg
RA of node: 91
7564 deg
Eccentricity:
0002520
Arg of perigee: 124
7904 deg
Mean anomaly: 235
3497 deg
Mean motion: 15
73788471 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3198
Checksum: 300
Coasting Arc #3 (Orbit 3213)
---------------------------------------
Vector Time (GMT): 2011/112/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2700368
99 A = 6728766
45 meter
Y = -5397737
34 meter E =
0015394
Z = 2957791
18 I = 51
99036
XDOT = 3618
096999 Wp = 101
97833
YDOT = -4577
791836 meter/sec RA = 85
94262 deg
ZDOT = -5032
178163 TA = 44
06822
MA = 43
94562
Ha = 191
069 n
mi
Hp = 183
296
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8859478
31 X = -2654178
21
Y = -17709112
00 feet Y = -5427676
34 meter
Z = 9704039
31 Z = 2944784
76
XDOT = 11870
396979 XDOT = 3693
463312
YDOT = -15019
002088 feet/sec YDOT = -4536
910510 meter/sec
ZDOT = -16509
770875 ZDOT = -5014
418495
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16464765
68 X = -5018460
58
Y = -11046715
62 feet Y = -3367038
92 meter
Z = 9651577
47 Z = 2941800
81
XDOT = 2244
501965 XDOT = 684
124199
YDOT = -17761
086996 feet/sec YDOT = -5413
579316 meter/sec
ZDOT = -16437
756302 ZDOT = -5010
228121
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 11112
53777306
00016717 00000-0 10270-3 0 9023
2 25544 51
6402 86
5408 0002345 128
7870 231
3503 15
73876075 32144
Satellite: ISS
Catalog Number: 25544
Epoch time: 11112
53777306 = yrday
fracday
Element set: 902
Inclination: 51
6402 deg
RA of node: 86
5408 deg
Eccentricity:
0002345
Arg of perigee: 128
7870 deg
Mean anomaly: 231
3503 deg
Mean motion: 15
73876075 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3214
Checksum: 291
Coasting Arc #4 (Orbit 3229)
---------------------------------------
Vector Time (GMT): 2011/113/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2775681
14 A = 6724004
82 meter
Y = 4282300
58 meter E =
0011652
Z = 4372187
03 I = 51
97258
XDOT = -3646
897890 Wp = 115
07941
YDOT = -5863
618093 meter/sec RA = 80
88077 deg
ZDOT = 3415
970760 TA = 300
60657
MA = 300
72143
Ha = 190
883 n
mi
Hp = 183
228
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9106565
43 X = -2844599
62
Y = 14049542
60 feet Y = 4250875
77 meter
Z = 14344445
64 Z = 4358535
50
XDOT = -11964
888090 XDOT = -3597
652896
YDOT = -19237
592168 feet/sec YDOT = -5904
124666 meter/sec
ZDOT = 11207
253149 ZDOT = 3398
373606
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -819019
06 X = -249637
01
Y = 16770044
46 feet Y = 5111509
55 meter
Z = 14289055
90 Z = 4355304
24
XDOT = -18889
070419 XDOT = -5757
388664
YDOT = -10444
531066 feet/sec YDOT = -3183
493069 meter/sec
ZDOT = 11136
231940 ZDOT = 3394
323495
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 11113
55366531
00016717 00000-0 10270-3 0 9031
2 25544 51
6409 81
3253 0002364 137
8516 222
2830 15
73969841 32305
Satellite: ISS
Catalog Number: 25544
Epoch time: 11113
55366531 = yrday
fracday
Element set: 903
Inclination: 51
6409 deg
RA of node: 81
3253 deg
Eccentricity:
0002364
Arg of perigee: 137
8516 deg
Mean anomaly: 222
2830 deg
Mean motion: 15
73969841 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3230
Checksum: 290
Coasting Arc #5 (Orbit 3244)
---------------------------------------
Vector Time (GMT): 2011/114/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3631562
44 A = 6728394
85 meter
Y = 4819311
59 meter E =
0005840
Z = -2981172
09 I = 51
98142
XDOT = -2733
067295 Wp = 90
50784
YDOT = 5156
259094 meter/sec RA = 75
72088 deg
ZDOT = 5014
532043 TA = 235
28244
MA = 235
33746
Ha = 190
799 n
mi
Hp = 183
235
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11914574
93 X = 3591884
01
Y = 15811389
73 feet Y = 4859700
10 meter
Z = -9780748
33 Z = -2963626
34
XDOT = -8966
756218 XDOT = -2814
882051
YDOT = 16916
860546 feet/sec YDOT = 5125
238767 meter/sec
ZDOT = 16451
876781 ZDOT = 5001
056180
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18455182
37 X = 5625139
59
Y = 7262521
16 feet Y = 2213616
45 meter
Z = -9709902
61 Z = -2959578
31
XDOT = 1601
010526 XDOT = 487
988008
YDOT = 17817
533359 feet/sec YDOT = 5430
784168 meter/sec
ZDOT = 16397
160795 ZDOT = 4997
854610
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 11114
50602516
00016717 00000-0 10270-3 0 9044
2 25544 51
6408 76
4346 0002378 137
1849 222
9500 15
73989732 32457
Satellite: ISS
Catalog Number: 25544
Epoch time: 11114
50602516 = yrday
fracday
Element set: 904
Inclination: 51
6408 deg
RA of node: 76
4346 deg
Eccentricity:
0002378
Arg of perigee: 137
1849 deg
Mean anomaly: 222
9500 deg
Mean motion: 15
73989732 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3245
Checksum: 305
Coasting Arc #6 (Orbit 3260)
---------------------------------------
Vector Time (GMT): 2011/115/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2016818
52 A = 6723555
92 meter
Y = -4667989
85 meter E =
0010181
Z = -4408119
28 I = 51
95813
XDOT = 4603
648902 Wp = 81
93100
YDOT = 5162
629630 meter/sec RA = 70
65588 deg
ZDOT = -3365
884479 TA = 154
34382
MA = 154
29327
Ha = 190
607 n
mi
Hp = 183
157
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6616858
66 X = 2090280
75
Y = -15314927
32 feet Y = -4645025
84 meter
Z = -14462333
58 Z = -4398143
14
XDOT = 15103
834979 XDOT = 4561
928032
YDOT = 16937
761252 feet/sec YDOT = 5213
877132 meter/sec
ZDOT = -11042
928081 ZDOT = -3343
621408
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2537970
92 X = -773573
54
Y = -16524512
19 feet Y = -5036671
31 meter
Z = -14421792
91 Z = -4395762
48
XDOT = 20675
419352 XDOT = 6301
867818
YDOT = 6368
871026 feet/sec YDOT = 1941
231889 meter/sec
ZDOT = -10953
004896 ZDOT = -3338
475892
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 11115
52182996
00016717 00000-0 10270-3 0 9053
2 25544 51
6416 71
2174 0002352 142
9089 217
2237 15
74080593 32610
Satellite: ISS
Catalog Number: 25544
Epoch time: 11115
52182996 = yrday
fracday
Element set: 905
Inclination: 51
6416 deg
RA of node: 71
2174 deg
Eccentricity:
0002352
Arg of perigee: 142
9089 deg
Mean anomaly: 217
2237 deg
Mean motion: 15
74080593 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3261
Checksum: 297
Coasting Arc #7 (Orbit 3276)
---------------------------------------
Vector Time (GMT): 2011/116/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4393170
90 A = 6728175
03 meter
Y = -4184019
39 meter E =
0015060
Z = 2891455
31 I = 51
96324
XDOT = 1867
849551 Wp = 105
20295
YDOT = -5484
432495 meter/sec RA = 65
49502 deg
ZDOT = -5080
272196 TA = 41
68670
MA = 41
57203
Ha = 190
499 n
mi
Hp = 183
086
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14413290
35 X = -4360104
01
Y = -13727097
74 feet Y = -4232961
54 meter
Z = 9486401
95 Z = 2870193
75
XDOT = 6128
115325 XDOT = 1953
717685
YDOT = -17993
544930 feet/sec YDOT = -5463
065063 meter/sec
ZDOT = -16667
559699 ZDOT = -5070
989513
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19633679
87 X = -5984345
62
Y = -3509581
80 feet Y = -1069720
53 meter
Z = 9400501
22 Z = 2865272
77
XDOT = -4947
797983 XDOT = -1508
088825
YDOT = -17022
702200 feet/sec YDOT = -5188
519630 meter/sec
ZDOT = -16629
791339 ZDOT = -5068
760400
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 11116
53758862
00016717 00000-0 10270-3 0 9067
2 25544 51
6418 66
0005 0002310 148
0318 212
0986 15
74151428 32770
Satellite: ISS
Catalog Number: 25544
Epoch time: 11116
53758862 = yrday
fracday
Element set: 906
Inclination: 51
6418 deg
RA of node: 66
0005 deg
Eccentricity:
0002310
Arg of perigee: 148
0318 deg
Mean anomaly: 212
0986 deg
Mean motion: 15
74151428 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3277
Checksum: 291
Coasting Arc #8 (Orbit 3292)
---------------------------------------
Vector Time (GMT): 2011/117/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1261905
34 A = 6722816
88 meter
Y = 4860834
47 meter E =
0010882
Z = 4464510
66 I = 51
93304
XDOT = -5423
502710 Wp = 120
84161
YDOT = -4402
242818 meter/sec RA = 60
42738 deg
ZDOT = 3248
806714 TA = 296
71460
MA = 296
82595
Ha = 190
239 n
mi
Hp = 183
017
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4140109
39 X = -1337854
13
Y = 15947619
65 feet Y = 4846298
57 meter
Z = 14647344
68 Z = 4458195
68
XDOT = -17793
644061 XDOT = -5389
655022
YDOT = -14443
053864 feet/sec YDOT = -4462
702359 meter/sec
ZDOT = 10658
814678 ZDOT = 3222
541689
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5505871
06 X = 1678189
50
Y = 15553321
90 feet Y = 4740652
51 meter
Z = 14621605
47 Z = 4456665
35
XDOT = -21757
720124 XDOT = -6631
753094
YDOT = -2253
103396 feet/sec YDOT = -686
745915 meter/sec
ZDOT = 10552
676995 ZDOT = 3216
455948
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 11117
55329924
00016717 00000-0 10270-3 0 9074
2 25544 51
6424 60
7835 0002404 157
3625 202
7645 15
74249834 32932
Satellite: ISS
Catalog Number: 25544
Epoch time: 11117
55329924 = yrday
fracday
Element set: 907
Inclination: 51
6424 deg
RA of node: 60
7835 deg
Eccentricity:
0002404
Arg of perigee: 157
3625 deg
Mean anomaly: 202
7645 deg
Mean motion: 15
74249834 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3293
Checksum: 310
Coasting Arc #9 (Orbit 3307)
---------------------------------------
Vector Time (GMT): 2011/118/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5048051
34 A = 6728160
88 meter
Y = 3495952
62 meter E =
0004863
Z = -2753658
31 I = 51
93482
XDOT = -1054
738035 Wp = 84
26185
YDOT = 5594
650329 meter/sec RA = 55
26404 deg
ZDOT = 5177
469694 TA = 244
42407
MA = 244
47435
Ha = 190
112 n
mi
Hp = 183
095
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16561848
23 X = 5021960
58
Y = 11469660
81 feet Y = 3552257
01 meter
Z = -9034312
03 Z = -2729198
27
XDOT = -3460
426625 XDOT = -1142
371412
YDOT = 18355
151999 feet/sec YDOT = 5582
365810 meter/sec
ZDOT = 16986
449126 ZDOT = 5172
132692
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20188157
95 X = 6153350
54
Y = -250391
97 feet Y = -76319
47 meter
Z = -8935452
55 Z = -2723525
94
XDOT = 7689
612173 XDOT = 2343
793790
YDOT = 15563
569046 feet/sec YDOT = 4743
775845 meter/sec
ZDOT = 16964
634556 ZDOT = 5170
820613
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 11118
50548779
00016717 00000-0 10270-3 0 9082
2 25544 51
6422 55
8916 0002275 159
9813 200
1440 15
74276126 33084
Satellite: ISS
Catalog Number: 25544
Epoch time: 11118
50548779 = yrday
fracday
Element set: 908
Inclination: 51
6422 deg
RA of node: 55
8916 deg
Eccentricity:
0002275
Arg of perigee: 159
9813 deg
Mean anomaly: 200
1440 deg
Mean motion: 15
74276126 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3308
Checksum: 310
Coasting Arc #10 (Orbit 3323)
---------------------------------------
Vector Time (GMT): 2011/119/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 625939
74 A = 6721959
10 meter
Y = -4875954
66 meter E =
0010560
Z = -4594167
00 I = 51
89760
XDOT = 6086
730763 Wp = 82
41502
YDOT = 3614
573893 meter/sec RA = 50
19054 deg
ZDOT = -3011
485446 TA = 157
77569
MA = 157
72988
Ha = 189
927 n
mi
Hp = 182
935
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2053608
08 X = 702734
90
Y = -15997226
58 feet Y = -4868525
79 meter
Z = -15072726
37 Z = -4590939
46
XDOT = 19969
589119 XDOT = 6060
488896
YDOT = 11858
838232 feet/sec YDOT = 3682
492587 meter/sec
ZDOT = -9880
201594 ZDOT = -2981
979728
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7746218
00 X = -2361047
25
Y = -14160653
11 feet Y = -4316167
07 meter
Z = -15059470
60 Z = -4590126
64
XDOT = 22128
690670 XDOT = 6744
824916
YDOT = -1740
167874 feet/sec YDOT = -530
403168 meter/sec
ZDOT = -9760
934806 ZDOT = -2975
132929
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 11119
52110888
00016717 00000-0 10270-3 0 9092
2 25544 51
6433 50
6732 0002327 163
5146 196
6093 15
74374341 33242
Satellite: ISS
Catalog Number: 25544
Epoch time: 11119
52110888 = yrday
fracday
Element set: 909
Inclination: 51
6433 deg
RA of node: 50
6732 deg
Eccentricity:
0002327
Arg of perigee: 163
5146 deg
Mean anomaly: 196
6093 deg
Mean motion: 15
74374341 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3324
Checksum: 298
Coasting Arc #11 (Orbit 3339)
---------------------------------------
Vector Time (GMT): 2011/120/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5572055
58 A = 6728307
16 meter
Y = -2808837
29 meter E =
0015043
Z = 2495383
74 I = 51
89925
XDOT = 389
889987 Wp = 112
80544
YDOT = -5538
330222 meter/sec RA = 45
02701 deg
ZDOT = -5343
774663 TA = 39
04002
MA = 38
93153
Ha = 189
833 n
mi
Hp = 182
937
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18281022
24 X = -5552354
76
Y = -9215345
44 feet Y = -2871037
19 meter
Z = 8186954
51 Z = 2468362
29
XDOT = 1279
166624 XDOT = 477
751082
YDOT = -18170
374743 feet/sec YDOT = -5533
479101 meter/sec
ZDOT = -17532
069104 ZDOT = -5341
667009
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20165128
25 X = -6146331
09
Y = 3776594
40 feet Y = 1151105
97 meter
Z = 8077717
95 Z = 2462088
43
XDOT = -9634
502596 XDOT = -2936
596391
YDOT = -13823
317573 feet/sec YDOT = -4213
347196 meter/sec
ZDOT = -17523
310863 ZDOT = -5341
105151
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 11120
53668311
00016717 00000-0 10270-3 0 9106
2 25544 51
6437 45
4553 0002363 169
7443 190
3769 15
74433713 33405
Satellite: ISS
Catalog Number: 25544
Epoch time: 11120
53668311 = yrday
fracday
Element set: 910
Inclination: 51
6437 deg
RA of node: 45
4553 deg
Eccentricity:
0002363
Arg of perigee: 169
7443 deg
Mean anomaly: 190
3769 deg
Mean motion: 15
74433713 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3340
Checksum: 295
Coasting Arc #12 (Orbit 3355)
---------------------------------------
Vector Time (GMT): 2011/121/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -93344
06 A = 6720946
98 meter
Y = 4769157
01 meter E =
0009143
Z = 4731414
04 I = 51
85316
XDOT = -6648
554290 Wp = 131
36216
YDOT = -2810
190495 meter/sec RA = 39
94703 deg
ZDOT = 2692
184328 TA = 292
20660
MA = 292
30357
Ha = 189
566 n
mi
Hp = 182
866
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -306246
92 X = -169651
45
Y = 15646840
59 feet Y = 4767686
57 meter
Z = 15523011
95 Z = 4730775
17
XDOT = -21812
842158 XDOT = -6629
714404
YDOT = -9219
785088 feet/sec YDOT = -2884
433301 meter/sec
ZDOT = 8832
625749 ZDOT = 2659
930953
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9381114
24 X = 2859363
62
Y = 12529913
18 feet Y = 3819117
54 meter
Z = 15520221
61 Z = 4730563
55
XDOT = -21961
522283 XDOT = -6693
871992
YDOT = 5625
868623 feet/sec YDOT = 1714
764756 meter/sec
ZDOT = 8702
225438 ZDOT = 2652
438314
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 11121
55220941
00016717 00000-0 10270-3 0 9113
2 25544 51
6439 40
2370 0002446 176
2421 183
8761 15
74520392 33564
Satellite: ISS
Catalog Number: 25544
Epoch time: 11121
55220941 = yrday
fracday
Element set: 911
Inclination: 51
6439 deg
RA of node: 40
2370 deg
Eccentricity:
0002446
Arg of perigee: 176
2421 deg
Mean anomaly: 183
8761 deg
Mean motion: 15
74520392 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3356
Checksum: 281
Coasting Arc #13 (Orbit 3370)
---------------------------------------
Vector Time (GMT): 2011/122/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6012063
03 A = 6728528
45 meter
Y = 2096012
57 meter E =
0004756
Z = -2175036
43 I = 51
85534
XDOT = 122
953096 Wp = 60
23880
YDOT = 5363
302682 meter/sec RA = 34
78280 deg
ZDOT = 5519
571934 TA = 275
49048
MA = 275
54473
Ha = 189
401 n
mi
Hp = 182
905
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19724616
26 X = 5998744
30
Y = 6876681
68 feet Y = 2163168
66 meter
Z = -7135946
29 Z = -2145861
66
XDOT = 403
389421 XDOT = 36
156940
YDOT = 17596
137407 feet/sec YDOT = 5364
192264 meter/sec
ZDOT = 18108
831803 ZDOT = 5519
958467
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19655735
99 X = 5991068
33
Y = -7188251
33 feet Y = -2190979
01 meter
Z = -7017980
64 Z = -2139080
50
XDOT = 10842
376911 XDOT = 3304
756482
YDOT = 12003
209760 feet/sec YDOT = 3658
578335 meter/sec
ZDOT = 18110
155889 ZDOT = 5519
975515
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 11122
50422368
00016717 00000-0 10270-3 0 9127
2 25544 51
6445 35
3444 0002399 181
2293 178
8865 15
74580511 33713
Satellite: ISS
Catalog Number: 25544
Epoch time: 11122
50422368 = yrday
fracday
Element set: 912
Inclination: 51
6445 deg
RA of node: 35
3444 deg
Eccentricity:
0002399
Arg of perigee: 181
2293 deg
Mean anomaly: 178
8865 deg
Mean motion: 15
74580511 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3371
Checksum: 304
Coasting Arc #14 (Orbit 3386)
---------------------------------------
Vector Time (GMT): 2011/123/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -249524
68 A = 6719789
34 meter
Y = -4590928
39 meter E =
0011870
Z = -4911192
72 I = 51
80174
XDOT = 7080
296847 Wp = 84
20253
YDOT = 2008
110970 meter/sec RA = 29
69333 deg
ZDOT = -2240
328949 TA = 164
06580
MA = 164
02843
Ha = 189
187 n
mi
Hp = 182
773
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -818650
54 X = -174311
39
Y = -15062101
00 feet Y = -4593298
04 meter
Z = -16112837
02 Z = -4912222
38
XDOT = 23229
320364 XDOT = 7068
198840
YDOT = 6588
290584 feet/sec YDOT = 2087
219569 meter/sec
ZDOT = -7350
160594 ZDOT = -2205
961591
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10284514
15 X = -3134719
91
Y = -11028981
64 feet Y = -3361633
60 meter
Z = -16116790
16 Z = -4912397
64
XDOT = 21214
219827 XDOT = 6466
094203
YDOT = -9260
922292 feet/sec YDOT = -2822
729115 meter/sec
ZDOT = -7211
184541 ZDOT = -2197
969048
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 11123
51965920
00016717 00000-0 10270-3 0 9136
2 25544 51
6452 30
1254 0002373 185
5584 174
5554 15
74669079 33877
Satellite: ISS
Catalog Number: 25544
Epoch time: 11123
51965920 = yrday
fracday
Element set: 913
Inclination: 51
6452 deg
RA of node: 30
1254 deg
Eccentricity:
0002373
Arg of perigee: 185
5584 deg
Mean anomaly: 174
5554 deg
Mean motion: 15
74669079 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3387
Checksum: 317
Coasting Arc #15 (Orbit 3402)
---------------------------------------
Vector Time (GMT): 2011/124/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6342681
82 A = 6728959
96 meter
Y = -1405880
38 meter E =
0014966
Z = 1721462
96 I = 51
80515
XDOT = -420
893898 Wp = 124
76743
YDOT = -5142
175568 meter/sec RA = 24
53099 deg
ZDOT = -5723
704477 TA = 36
21172
MA = 36
11050
Ha = 189
121 n
mi
Hp = 182
855
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20809323
56 X = -6334852
28
Y = -4612468
45 feet Y = -1476764
41 meter
Z = 5647844
36 Z = 1690668
65
XDOT = -1380
885491 XDOT = -335
556646
YDOT = -16870
654750 feet/sec YDOT = -5146
404824 meter/sec
ZDOT = -18778
557995 ZDOT = -5725
542184
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18713203
94 X = -5703784
56
Y = 10271810
49 feet Y = 3130847
84 meter
Z = 5523302
07 Z = 1683502
47
XDOT = -11326
743764 XDOT = -3452
391499
YDOT = -10485
788103 feet/sec YDOT = -3196
068214 meter/sec
ZDOT = -18785
746930 ZDOT = -5725
895664
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
53504881
00016717 00000-0 10270-3 0 9145
2 25544 51
6449 24
9062 0002516 190
9632 169
1477 15
74698547 34039
Satellite: ISS
Catalog Number: 25544
Epoch time: 11124
53504881 = yrday
fracday
Element set: 914
Inclination: 51
6449 deg
RA of node: 24
9062 deg
Eccentricity:
0002516
Arg of perigee: 190
9632 deg
Mean anomaly: 169
1477 deg
Mean motion: 15
74698547 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3403
Checksum: 318
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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