[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
April 10th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 20451 43 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 94 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 922 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 2992)
---------------------------------------
Vector Time (GMT): 2011/098/11:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4332427
09 A = 6725787
80 meter
Y = 2193770
48 meter E =
0012808
Z = -4665507
18 I = 51
75963
XDOT = -5418
321619 Wp = 74
17743
YDOT = 4653
669296 meter/sec RA = 157
64488 deg
ZDOT = -2846
320034 TA = 167
71738
MA = 167
68613
Ha = 192
500 n
mi
Hp = 184
659
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14213999
65 X = 4330238
25
Y = 7197409
70 feet Y = 2242205
95 meter
Z = -15306782
08 Z = -4644465
50
XDOT = -17776
645730 XDOT = -5456
130145
YDOT = 15267
943884 feet/sec YDOT = 4592
866869 meter/sec
ZDOT = -9338
320322 ZDOT = -2872
734338
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15220265
80 X = 4639137
02
Y = 4977955
34 feet Y = 1517280
79 meter
Z = -15221745
62 Z = -4639588
06
XDOT = -14876
617120 XDOT = -4534
392898
YDOT = 16634
600298 feet/sec YDOT = 5070
226171 meter/sec
ZDOT = -9445
159481 ZDOT = -2878
884610
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 11098
50150367
00016717 00000-0 10270-3 0 9003
2 25544 51
6431 158
5521 0002206 90
7909 269
3506 15
72967958 29936
Satellite: ISS
Catalog Number: 25544
Epoch time: 11098
50150367 = yrday
fracday
Element set: 900
Inclination: 51
6431 deg
RA of node: 158
5521 deg
Eccentricity:
0002206
Arg of perigee: 90
7909 deg
Mean anomaly: 269
3506 deg
Mean motion: 15
72967958 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2993
Checksum: 323
Coasting Arc #2 (Orbit 3008)
---------------------------------------
Vector Time (GMT): 2011/099/11:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4092229
10 A = 6731447
16 meter
Y = -4572208
49 meter E =
0015750
Z = 2751135
70 I = 51
80850
XDOT = 5440
508929 Wp = 98
82831
YDOT = 1747
666539 meter/sec RA = 152
48256 deg
ZDOT = -5165
452898 TA = 49
80340
MA = 49
66565
Ha = 192
294 n
mi
Hp = 184
352
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13425948
51 X = 4129687
72
Y = -15000684
01 feet Y = -4526237
21 meter
Z = 9026035
76 Z = 2771106
86
XDOT = 17849
438743 XDOT = 5445
654729
YDOT = 5733
814103 feet/sec YDOT = 1808
534289 meter/sec
ZDOT = -16947
023942 ZDOT = -5139
010378
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10688517
53 X = 3257860
14
Y = -17016667
55 feet Y = -5186680
27 meter
Z = 9106841
05 Z = 2775765
15
XDOT = 17413
503615 XDOT = 5307
635902
YDOT = 1886
034190 feet/sec YDOT = 574
863221 meter/sec
ZDOT = -16840
137356 ZDOT = -5132
873866
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 11099
51796874
00016717 00000-0 10270-3 0 9015
2 25544 51
6437 153
3399 0002236 88
0689 272
0730 15
73081383 30095
Satellite: ISS
Catalog Number: 25544
Epoch time: 11099
51796874 = yrday
fracday
Element set: 901
Inclination: 51
6437 deg
RA of node: 153
3399 deg
Eccentricity:
0002236
Arg of perigee: 88
0689 deg
Mean anomaly: 272
0730 deg
Mean motion: 15
73081383 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3009
Checksum: 324
Coasting Arc #3 (Orbit 3024)
---------------------------------------
Vector Time (GMT): 2011/100/11:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5062178
70 A = 6726564
34 meter
Y = -819772
46 meter E =
0011960
Z = 4345183
55 I = 51
81852
XDOT = 3884
627912 Wp = 106
18764
YDOT = -5693
943712 meter/sec RA = 147
41386 deg
ZDOT = 3440
348425 TA = 309
13930
MA = 309
24554
Ha = 192
417 n
mi
Hp = 184
283
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16608197
84 X = -5073743
70
Y = -2689542
19 feet Y = -876445
39 meter
Z = 14255851
53 Z = 4320563
44
XDOT = 12744
842232 XDOT = 3931
297392
YDOT = -18680
917689 feet/sec YDOT = -5650
242440 meter/sec
ZDOT = 11287
232365 ZDOT = 3459
333386
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16903239
84 X = -5152107
50
Y = 417798
41 feet Y = 127344
96 meter
Z = 14156309
66 Z = 4314843
18
XDOT = 9066
987776 XDOT = 2763
617874
YDOT = -19455
757715 feet/sec YDOT = -5930
114952 meter/sec
ZDOT = 11364
078735 ZDOT = 3463
771198
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 11100
53439310
00016717 00000-0 10270-3 0 9020
2 25544 51
6433 148
1275 0002341 93
8368 266
3062 15
73126548 30256
Satellite: ISS
Catalog Number: 25544
Epoch time: 11100
53439310 = yrday
fracday
Element set: 902
Inclination: 51
6433 deg
RA of node: 148
1275 deg
Eccentricity:
0002341
Arg of perigee: 93
8368 deg
Mean anomaly: 266
3062 deg
Mean motion: 15
73126548 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3025
Checksum: 280
Coasting Arc #4 (Orbit 3039)
---------------------------------------
Vector Time (GMT): 2011/101/11:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2668534
93 A = 6729871
42 meter
Y = 5271765
70 meter E =
0007110
Z = -3227357
06 I = 51
85598
XDOT = -6011
799242 Wp = 87
81552
YDOT = -111
196721 meter/sec RA = 142
24968 deg
ZDOT = 4798
518590 TA = 234
63001
MA = 234
69647
Ha = 192
223 n
mi
Hp = 184
061
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8755035
85 X = -2711608
64
Y = 17295819
24 feet Y = 5241683
60 meter
Z = -10588441
79 Z = -3240425
51
XDOT = -19723
750793 XDOT = -6033
419242
YDOT = -364
818637 feet/sec YDOT = -178
545063 meter/sec
ZDOT = 15743
171228 ZDOT = 4769
260887
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5051870
25 X = -1539810
05
Y = 18685583
17 feet Y = 5695365
75 meter
Z = -10641367
58 Z = -3243488
84
XDOT = -18126
529643 XDOT = -5524
966235
YDOT = 3980
265919 feet/sec YDOT = 1213
185052 meter/sec
ZDOT = 15624
853517 ZDOT = 4762
455352
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 11101
48725334
00016717 00000-0 10270-3 0 9030
2 25544 51
6434 143
2406 0002510 95
6346 264
5103 15
73204163 30406
Satellite: ISS
Catalog Number: 25544
Epoch time: 11101
48725334 = yrday
fracday
Element set: 903
Inclination: 51
6434 deg
RA of node: 143
2406 deg
Eccentricity:
0002510
Arg of perigee: 95
6346 deg
Mean anomaly: 264
5103 deg
Mean motion: 15
73204163 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3040
Checksum: 260
Coasting Arc #5 (Orbit 3055)
---------------------------------------
Vector Time (GMT): 2011/102/11:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5340424
18 A = 6727308
41 meter
Y = -609092
63 meter E =
0009585
Z = -4054850
06 I = 51
87186
XDOT = -2240
405160 Wp = 78
46622
YDOT = 6242
343072 meter/sec RA = 137
18637 deg
ZDOT = -3894
247193 TA = 151
49330
MA = 151
44085
Ha = 192
208 n
mi
Hp = 184
125
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17521076
72 X = 5366535
87
Y = -1998335
40 feet Y = -549226
94 meter
Z = -13303313
85 Z = -4028842
99
XDOT = -7350
410630 XDOT = -2291
124281
YDOT = 20480
128189 feet/sec YDOT = 6217
005756 meter/sec
ZDOT = -12776
401553 ZDOT = -3905
254470
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16746752
88 X = 5104410
28
Y = -5771959
20 feet Y = -1759293
17 meter
Z = -13198120
62 Z = -4022787
17
XDOT = -3075
472017 XDOT = -937
403871
YDOT = 20349
052776 feet/sec YDOT = 6202
391286 meter/sec
ZDOT = -12821
013167 ZDOT = -3907
844813
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 11102
50359629
00016717 00000-0 10270-3 0 9045
2 25544 51
6442 138
0274 0002546 97
5026 262
6427 15
73243773 30560
Satellite: ISS
Catalog Number: 25544
Epoch time: 11102
50359629 = yrday
fracday
Element set: 904
Inclination: 51
6442 deg
RA of node: 138
0274 deg
Eccentricity:
0002546
Arg of perigee: 97
5026 deg
Mean anomaly: 262
6427 deg
Mean motion: 15
73243773 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3056
Checksum: 299
Coasting Arc #6 (Orbit 3071)
---------------------------------------
Vector Time (GMT): 2011/103/11:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1242456
99 A = 6728517
11 meter
Y = -5559290
87 meter E =
0014571
Z = 3568842
99 I = 51
89783
XDOT = 6087
878167 Wp = 88
72124
YDOT = -1519
373974 meter/sec RA = 132
02289 deg
ZDOT = -4470
300759 TA = 48
84928
MA = 48
72364
Ha = 192
033 n
mi
Hp = 183
891
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4076302
45 X = 1287193
00
Y = -18239143
28 feet Y = -5545146
62 meter
Z = 11708802
45 Z = 3574987
81
XDOT = 19973
353566 XDOT = 6126
131425
YDOT = -4984
822749 feet/sec YDOT = -1451
082010 meter/sec
ZDOT = -14666
341074 ZDOT = -4440
633006
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -369894
46 X = -112743
83
Y = -18669791
35 feet Y = -5690552
40 meter
Z = 11733742
50 Z = 3576444
71
XDOT = 16977
367028 XDOT = 5174
701470
YDOT = -9511
280608 feet/sec YDOT = -2899
038329 meter/sec
ZDOT = -14546
318387 ZDOT = -4433
717844
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 11103
51989571
00016717 00000-0 10270-3 0 9053
2 25544 51
6434 132
8144 0002514 98
1946 261
9502 15
73331656 30724
Satellite: ISS
Catalog Number: 25544
Epoch time: 11103
51989571 = yrday
fracday
Element set: 905
Inclination: 51
6434 deg
RA of node: 132
8144 deg
Eccentricity:
0002514
Arg of perigee: 98
1946 deg
Mean anomaly: 261
9502 deg
Mean motion: 15
73331656 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3072
Checksum: 301
Coasting Arc #7 (Orbit 3087)
---------------------------------------
Vector Time (GMT): 2011/104/11:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5199148
21 A = 6727977
97 meter
Y = 2018249
28 meter E =
0014439
Z = 3752481
29 I = 51
91532
XDOT = 615
431817 Wp = 97
42969
YDOT = -6382
757489 meter/sec RA = 126
96265 deg
ZDOT = 4269
878499 TA = 307
74281
MA = 307
87357
Ha = 192
167 n
mi
Hp = 183
809
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17057572
86 X = -5239559
07
Y = 6621552
75 feet Y = 1959883
59 meter
Z = 12311290
32 Z = 3727125
59
XDOT = 2019
133257 XDOT = 666
017048
YDOT = -20940
805410 feet/sec YDOT = -6375
592185 meter/sec
ZDOT = 14008
787726 ZDOT = 4272
991629
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14925590
30 X = -4549319
92
Y = 10702717
85 feet Y = 3262188
40 meter
Z = 12208693
90 Z = 3721209
90
XDOT = -2592
216402 XDOT = -790
107559
YDOT = -19668
859947 feet/sec YDOT = -5995
068512 meter/sec
ZDOT = 14021
482744 ZDOT = 4273
747940
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 11104
53615478
00016717 00000-0 10270-3 0 9069
2 25544 51
6429 127
6005 0002723 101
0155 259
1314 15
73359945 30882
Satellite: ISS
Catalog Number: 25544
Epoch time: 11104
53615478 = yrday
fracday
Element set: 906
Inclination: 51
6429 deg
RA of node: 127
6005 deg
Eccentricity:
0002723
Arg of perigee: 101
0155 deg
Mean anomaly: 259
1314 deg
Mean motion: 15
73359945 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3088
Checksum: 295
Coasting Arc #8 (Orbit 3102)
---------------------------------------
Vector Time (GMT): 2011/105/11:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 138363
18 A = 6727302
83 meter
Y = 5514300
10 meter E =
0009100
Z = -3860423
02 I = 51
93252
XDOT = -5713
797959 Wp = 105
51444
YDOT = 3045
571263 meter/sec RA = 121
80044 deg
ZDOT = 4151
246334 TA = 207
74121
MA = 207
78978
Ha = 191
900 n
mi
Hp = 183
716
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 453947
44 X = 95444
22
Y = 18091535
77 feet Y = 5515607
05 meter
Z = -12665429
84 Z = -3859855
59
XDOT = -18746
056297 XDOT = -5767
595499
YDOT = 9992
031703 feet/sec YDOT = 2981
375676 meter/sec
ZDOT = 13619
574586 ZDOT = 4123
357710
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5343470
83 X = 1628689
91
Y = 17291986
81 feet Y = 5270597
58 meter
Z = -12663228
64 Z = -3859752
09
XDOT = -14212
534511 XDOT = -4331
980519
YDOT = 14269
413296 feet/sec YDOT = 4349
317173 meter/sec
ZDOT = 13506
708236 ZDOT = 4116
844670
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 11105
48885657
00016717 00000-0 10270-3 0 9073
2 25544 51
6439 122
7128 0002629 104
0607 256
0849 15
73440347 31039
Satellite: ISS
Catalog Number: 25544
Epoch time: 11105
48885657 = yrday
fracday
Element set: 907
Inclination: 51
6439 deg
RA of node: 122
7128 deg
Eccentricity:
0002629
Arg of perigee: 104
0607 deg
Mean anomaly: 256
0849 deg
Mean motion: 15
73440347 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3103
Checksum: 306
Coasting Arc #9 (Orbit 3118)
---------------------------------------
Vector Time (GMT): 2011/106/11:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4726277
02 A = 6728272
73 meter
Y = -3246457
71 meter E =
0007610
Z = -3526367
46 I = 51
95039
XDOT = 862
014799 Wp = 93
27833
YDOT = 6161
315292 meter/sec RA = 116
74110 deg
ZDOT = -4525
682169 TA = 128
42269
MA = 128
35434
Ha = 191
808 n
mi
Hp = 183
717
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15506158
19 X = 4779358
85
Y = -10651107
98 feet Y = -3193309
12 meter
Z = -11569447
06 Z = -3503277
82
XDOT = 2828
132543 XDOT = 815
038846
YDOT = 20214
289016 feet/sec YDOT = 6170
691822 meter/sec
ZDOT = -14848
038613 ZDOT = -4521
609101
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11913587
41 X = 3631261
44
Y = -14632409
73 feet Y = -4459958
49 meter
Z = -11475982
25 Z = -3497879
39
XDOT = 7464
415013 XDOT = 2275
153696
YDOT = 17687
006388 feet/sec YDOT = 5390
999547 meter/sec
ZDOT = -14831
676462 ZDOT = -4520
694986
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 11106
50503033
00016717 00000-0 10270-3 0 9083
2 25544 51
6429 117
4980 0002605 109
0705 251
0740 15
73504227 31193
Satellite: ISS
Catalog Number: 25544
Epoch time: 11106
50503033 = yrday
fracday
Element set: 908
Inclination: 51
6429 deg
RA of node: 117
4980 deg
Eccentricity:
0002605
Arg of perigee: 109
0705 deg
Mean anomaly: 251
0740 deg
Mean motion: 15
73504227 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3119
Checksum: 270
Coasting Arc #10 (Orbit 3134)
---------------------------------------
Vector Time (GMT): 2011/107/11:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1344802
36 A = 6726243
68 meter
Y = -5198138
25 meter E =
0012989
Z = 4041296
05 I = 51
95615
XDOT = 5013
521581 Wp = 83
85336
YDOT = -4349
093145 meter/sec RA = 111
57970 deg
ZDOT = -3913
685346 TA = 46
36408
MA = 46
25644
Ha = 191
669 n
mi
Hp = 183
515
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4412081
25 X = -1306207
98
Y = -17054259
36 feet Y = -5212960
58 meter
Z = 13258845
30 Z = 4034857
01
XDOT = 16448
561619 XDOT = 5080
793575
YDOT = -14268
678296 feet/sec YDOT = -4292
653029 meter/sec
ZDOT = -12840
175021 ZDOT = -3889
165649
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9402747
90 X = -2865957
56
Y = -14919443
09 feet Y = -4547446
25 meter
Z = 13232904
12 Z = 4033389
17
XDOT = 10392
597258 XDOT = 3167
663644
YDOT = -17885
482523 feet/sec YDOT = -5451
495073 meter/sec
ZDOT = -12740
892641 ZDOT = -3883
424077
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 11107
52115976
00016717 00000-0 10270-3 0 9092
2 25544 51
6417 112
2830 0002585 111
0571 249
0869 15
73596541 31355
Satellite: ISS
Catalog Number: 25544
Epoch time: 11107
52115976 = yrday
fracday
Element set: 909
Inclination: 51
6417 deg
RA of node: 112
2830 deg
Eccentricity:
0002585
Arg of perigee: 111
0571 deg
Mean anomaly: 249
0869 deg
Mean motion: 15
73596541 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3135
Checksum: 301
Coasting Arc #11 (Orbit 3150)
---------------------------------------
Vector Time (GMT): 2011/108/11:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3976905
66 A = 6728480
55 meter
Y = 4286789
37 meter E =
0015063
Z = 3316684
34 I = 51
97387
XDOT = -2169
186612 Wp = 93
06489
YDOT = -5683
686137 meter/sec RA = 106
52085 deg
ZDOT = 4726
055249 TA = 305
71385
MA = 305
85390
Ha = 191
588 n
mi
Hp = 183
498
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13047590
74 X = -4040657
89
Y = 14064269
59 feet Y = 4241960
87 meter
Z = 10881510
31 Z = 3297209
21
XDOT = -7116
753977 XDOT = -2128
428009
YDOT = -18647
264229 feet/sec YDOT = -5707
715221 meter/sec
ZDOT = 15505
430608 ZDOT = 4715
616402
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7986915
90 X = -2434411
97
Y = 17491800
40 feet Y = 5331500
76 meter
Z = 10802622
98 Z = 3292639
48
XDOT = -11464
969532 XDOT = -3494
522713
YDOT = -14823
827469 feet/sec YDOT = -4518
302612 meter/sec
ZDOT = 15463
330439 ZDOT = 4713
223118
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 11108
53724577
00016717 00000-0 10270-3 0 9109
2 25544 51
6413 107
0681 0002566 116
0877 244
0551 15
73643221 31519
Satellite: ISS
Catalog Number: 25544
Epoch time: 11108
53724577 = yrday
fracday
Element set: 910
Inclination: 51
6413 deg
RA of node: 107
0681 deg
Eccentricity:
0002566
Arg of perigee: 116
0877 deg
Mean anomaly: 244
0551 deg
Mean motion: 15
73643221 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3151
Checksum: 282
Coasting Arc #12 (Orbit 3165)
---------------------------------------
Vector Time (GMT): 2011/109/11:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2396726
66 A = 6725516
96 meter
Y = 4695386
04 meter E =
0010511
Z = -4187267
72 I = 51
97231
XDOT = -4047
354526 Wp = 112
16438
YDOT = 5379
226730 meter/sec RA = 101
36105 deg
ZDOT = 3718
862931 TA = 195
68906
MA = 195
72166
Ha = 191
434 n
mi
Hp = 183
501
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7863276
44 X = 2364385
12
Y = 15404809
85 feet Y = 4722006
83 meter
Z = -13737754
97 Z = -4175702
84
XDOT = -13278
722198 XDOT = -4125
271092
YDOT = 17648
381659 feet/sec YDOT = 5333
531130 meter/sec
ZDOT = 12200
993868 ZDOT = 3699
011282
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12618631
40 X = 3846158
85
Y = 11882319
04 feet Y = 3621730
84 meter
Z = -13691085
80 Z = -4173042
95
XDOT = -5851
077329 XDOT = -1783
408370
YDOT = 20165
876057 feet/sec YDOT = 6146
559022 meter/sec
ZDOT = 12120
539698 ZDOT = 3694
340500
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 11109
48978508
00016717 00000-0 10270-3 0 9110
2 25544 51
6417 102
1788 0002527 118
6437 241
4981 15
73684627 31663
Satellite: ISS
Catalog Number: 25544
Epoch time: 11109
48978508 = yrday
fracday
Element set: 911
Inclination: 51
6417 deg
RA of node: 102
1788 deg
Eccentricity:
0002527
Arg of perigee: 118
6437 deg
Mean anomaly: 241
4981 deg
Mean motion: 15
73684627 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3166
Checksum: 327
Coasting Arc #13 (Orbit 3181)
---------------------------------------
Vector Time (GMT): 2011/110/11:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3082111
53 A = 6728415
00 meter
Y = -5048333
37 meter E =
0007033
Z = -3210493
15 I = 51
98720
XDOT = 3239
734224 Wp = 108
18161
YDOT = 5041
170381 meter/sec RA = 96
30060 deg
ZDOT = -4827
517885 TA = 109
08210
MA = 109
00593
Ha = 191
329 n
mi
Hp = 183
384
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10111914
47 X = 3153930
07
Y = -16562773
53 feet Y = -5013465
72 meter
Z = -10533114
02 Z = -3195345
72
XDOT = 10629
049291 XDOT = 3206
573595
YDOT = 16539
272905 feet/sec YDOT = 5077
213728 meter/sec
ZDOT = -15838
313271 ZDOT = -4811
859529
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3755630
70 X = 1144716
24
Y = -19072541
49 feet Y = -5813310
65 meter
Z = -10471684
27 Z = -3191769
36
XDOT = 14429
865307 XDOT = 4398
222946
YDOT = 11483
238085 feet/sec YDOT = 3500
090968 meter/sec
ZDOT = -15775
098911 ZDOT = -4808
250148
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
50578341
00016717 00000-0 10270-3 0 9127
2 25544 51
6411 96
9625 0002594 123
5552 236
5859 15
73765245 31827
Satellite: ISS
Catalog Number: 25544
Epoch time: 11110
50578341 = yrday
fracday
Element set: 912
Inclination: 51
6411 deg
RA of node: 96
9625 deg
Eccentricity:
0002594
Arg of perigee: 123
5552 deg
Mean anomaly: 236
5859 deg
Mean motion: 15
73765245 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3182
Checksum: 308
Coasting Arc #14 (Orbit 3197)
---------------------------------------
Vector Time (GMT): 2011/111/11:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3235571
90 A = 6724822
10 meter
Y = -4085239
01 meter E =
0011629
Z = 4241346
98 I = 51
97823
XDOT = 2959
031445 Wp = 83
07797
YDOT = -6120
159561 meter/sec RA = 91
14129 deg
ZDOT = -3627
767004 TA = 43
66930
MA = 43
57734
Ha = 191
170 n
mi
Hp = 183
292
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10615393
36 X = -3210253
35
Y = -13403015
12 feet Y = -4121279
71 meter
Z = 13915180
36 Z = 4225689
82
XDOT = 9708
108414 XDOT = 3044
871480
YDOT = -20079
263650 feet/sec YDOT = -6086
589802 meter/sec
ZDOT = -11902
122718 ZDOT = -3613
183615
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14852386
31 X = -4527007
35
Y = -8572619
28 feet Y = -2612934
36 meter
Z = 13851947
69 Z = 4222073
66
XDOT = 1149
992924 XDOT = 350
517843
YDOT = -21180
790707 feet/sec YDOT = -6455
905007 meter/sec
ZDOT = -11842
927709 ZDOT = -3609
724366
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
52173462
00016717 00000-0 10270-3 0 9136
2 25544 51
6412 91
7469 0002420 128
0478 232
0904 15
73856223 31988
Satellite: ISS
Catalog Number: 25544
Epoch time: 11111
52173462 = yrday
fracday
Element set: 913
Inclination: 51
6412 deg
RA of node: 91
7469 deg
Eccentricity:
0002420
Arg of perigee: 128
0478 deg
Mean anomaly: 232
0904 deg
Mean motion: 15
73856223 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3198
Checksum: 288
Coasting Arc #15 (Orbit 3213)
---------------------------------------
Vector Time (GMT): 2011/112/11:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 893694
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2076323
79 A = 6728059
63 meter
Y = 5571165
12 meter E =
0014758
Z = 3137554
06 I = 51
98988
XDOT = -4121
873095 Wp = 92
98551
YDOT = -4299
085866 meter/sec RA = 86
08119 deg
ZDOT = 4885
581281 TA = 303
33881
MA = 303
48001
Ha = 190
919 n
mi
Hp = 183
207
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6812085
93 X = -2153709
02
Y = 18278100
79 feet Y = 5547513
61 meter
Z = 10293812
53 Z = 3127279
48
XDOT = -13523
205691 XDOT = -4097
226881
YDOT = -14104
612421 feet/sec YDOT = -4345
041517 meter/sec
ZDOT = 16028
809976 ZDOT = 4865
616882
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 608369
44 X = 185431
00
Y = 19518741
68 feet Y = 5949312
46 meter
Z = 10252056
84 Z = 3124826
93
XDOT = -16541
756976 XDOT = -5041
927526
YDOT = -7896
237752 feet/sec YDOT = -2406
773267 meter/sec
ZDOT = 15948
155926 ZDOT = 4860
997926
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
53763874
00016717 00000-0 10270-3 0 9141
2 25544 51
6415 86
5315 0002484 136
2624 223
8736 15
73955558 32148
Satellite: ISS
Catalog Number: 25544
Epoch time: 11112
53763874 = yrday
fracday
Element set: 914
Inclination: 51
6415 deg
RA of node: 86
5315 deg
Eccentricity:
0002484
Arg of perigee: 136
2624 deg
Mean anomaly: 223
8736 deg
Mean motion: 15
73955558 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3214
Checksum: 313
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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