[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
August 28th 2011
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) : 105 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 169 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 3711)
---------------------------------------
Vector Time (GMT): 2011/238/12:13:08
006
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1968209
69 A = 6759016
15 meter
Y = 3787742
86 meter E =
0025625
Z = -5261821
23 I = 51
70110
XDOT = -7178
041668 Wp = 99
37943
YDOT = 2530
360007 meter/sec RA = 165
76804 deg
ZDOT = -871
181616 TA = 162
33335
MA = 162
24407
Ha = 215
328 n
mi
Hp = 200
452
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6457380
88 X = 1951268
56
Y = 12426977
89 feet Y = 3809657
83 meter
Z = -17263193
00 Z = -5252301
04
XDOT = -23550
005471 XDOT = -7201
571207
YDOT = 8301
706060 feet/sec YDOT = 2449
959196 meter/sec
ZDOT = -2858
207400 ZDOT = -906
108960
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1158129
06 X = -352997
74
Y = -14004221
00 feet Y = -4268486
56 meter
Z = -17224572
89 Z = -5250049
82
XDOT = 23881
169092 XDOT = 7278
980339
YDOT = 1684
353383 feet/sec YDOT = 513
390911 meter/sec
ZDOT = -3000
427464 ZDOT = -914
530291
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 11238
52673992
00016717 00000-0 10270-3 0 9005
2 25544 51
6388 166
7268 0012354 117
8864 242
3544 15
60546032 37128
Satellite: ISS
Catalog Number: 25544
Epoch time: 11238
52673992 = yrday
fracday
Element set: 900
Inclination: 51
6388 deg
RA of node: 166
7268 deg
Eccentricity:
0012354
Arg of perigee: 117
8864 deg
Mean anomaly: 242
3544 deg
Mean motion: 15
60546032 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3712
Checksum: 317
Coasting Arc #2 (Orbit 3727)
---------------------------------------
Vector Time (GMT): 2011/239/12:13:08
006
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2357291
73 A = 6762227
34 meter
Y = -4520974
82 meter E =
0019329
Z = 4423773
34 I = 51
74159
XDOT = 6927
412756 Wp = 99
83514
YDOT = 351
709796 meter/sec RA = 160
71068 deg
ZDOT = -3322
903666 TA = 23
59060
MA = 23
50207
Ha = 215
218 n
mi
Hp = 200
470
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7733896
75 X = 2386181
54
Y = -14832594
55 feet Y = -4494452
47 meter
Z = 14513692
05 Z = 4435295
12
XDOT = 22727
732140 XDOT = 6939
106714
YDOT = 1153
903530 feet/sec YDOT = 429
241635 meter/sec
ZDOT = -10901
914915 ZDOT = -3289
222656
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12668792
72 X = -3861448
02
Y = 10860622
80 feet Y = 3310317
83 meter
Z = 14560729
40 Z = 4438110
32
XDOT = -19888
786860 XDOT = -6062
102235
YDOT = -8727
989879 feet/sec YDOT = -2660
291315 meter/sec
ZDOT = -10764
845171 ZDOT = -3281
124808
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 11239
55133041
00016717 00000-0 10270-3 0 9016
2 25544 51
6390 161
5698 0012335 121
6982 238
5379 15
60565238 37283
Satellite: ISS
Catalog Number: 25544
Epoch time: 11239
55133041 = yrday
fracday
Element set: 901
Inclination: 51
6390 deg
RA of node: 161
5698 deg
Eccentricity:
0012335
Arg of perigee: 121
6982 deg
Mean anomaly: 238
5379 deg
Mean motion: 15
60565238 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3728
Checksum: 313
Coasting Arc #3 (Orbit 3742)
---------------------------------------
Vector Time (GMT): 2011/240/12:13:08
006
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5516407
79 A = 6769748
47 meter
Y = 3680071
67 meter E =
0015212
Z = -1376631
79 I = 51
79577
XDOT = -3684
975792 Wp = 91
46199
YDOT = -3365
609463 meter/sec RA = 155
69578 deg
ZDOT = 5824
332257 TA = 253
54704
MA = 253
71427
Ha = 215
122 n
mi
Hp = 200
561
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18098450
77 X = -5550461
79
Y = 12073725
96 feet Y = 3618193
34 meter
Z = -4516508
48 Z = -1403512
87
XDOT = -12089
815592 XDOT = -3675
359982
YDOT = -11042
025796 feet/sec YDOT = -3406
763005 meter/sec
ZDOT = 19108
701631 ZDOT = 5806
454573
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21208748
77 X = 6464426
63
Y = -4745141
26 feet Y = -1446319
06 meter
Z = -4626039
08 Z = -1410016
71
XDOT = 7056
356395 XDOT = 2150
777429
YDOT = 13152
633277 feet/sec YDOT = 4008
922623 meter/sec
ZDOT = 19036
039206 ZDOT = 5802
184750
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 11240
51186773
00016717 00000-0 10270-3 0 9025
2 25544 51
6396 156
7343 0012244 125
3979 234
8322 15
60590926 37434
Satellite: ISS
Catalog Number: 25544
Epoch time: 11240
51186773 = yrday
fracday
Element set: 902
Inclination: 51
6396 deg
RA of node: 156
7343 deg
Eccentricity:
0012244
Arg of perigee: 125
3979 deg
Mean anomaly: 234
8322 deg
Mean motion: 15
60590926 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3743
Checksum: 313
Coasting Arc #4 (Orbit 3758)
---------------------------------------
Vector Time (GMT): 2011/241/12:13:08
006
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6181013
20 A = 6768077
08 meter
Y = -1266679
32 meter E =
0017768
Z = -2441038
13 I = 51
81824
XDOT = -998
367109 Wp = 131
01839
YDOT = 5399
061708 meter/sec RA = 150
70570 deg
ZDOT = -5366
333504 TA = 76
30614
MA = 76
10838
Ha = 215
105 n
mi
Hp = 200
704
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20278914
69 X = 6206575
99
Y = -4155772
04 feet Y = -1197416
71 meter
Z = -8008655
28 Z = -2410949
08
XDOT = -3275
482641 XDOT = -1032
598026
YDOT = 17713
457046 feet/sec YDOT = 5387
705541 meter/sec
ZDOT = -17606
081051 ZDOT = -5371
267058
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20514347
57 X = -6252773
14
Y = -3100613
36 feet Y = -945066
95 meter
Z = -7886134
81 Z = -2403693
89
XDOT = 8851
059934 XDOT = 2697
803068
YDOT = -14040
703976 feet/sec YDOT = -4279
606572 meter/sec
ZDOT = -17626
332820 ZDOT = -5372
506243
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 11241
53642423
00016717 00000-0 10270-3 0 9038
2 25544 51
6405 151
5761 0012213 129
5786 230
6450 15
60610048 37591
Satellite: ISS
Catalog Number: 25544
Epoch time: 11241
53642423 = yrday
fracday
Element set: 903
Inclination: 51
6405 deg
RA of node: 151
5761 deg
Eccentricity:
0012213
Arg of perigee: 129
5786 deg
Mean anomaly: 230
6450 deg
Mean motion: 15
60610048 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3759
Checksum: 283
Coasting Arc #5 (Orbit 3774)
---------------------------------------
Vector Time (GMT): 2011/242/12:13:08
006
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4200486
85 A = 6760006
81 meter
Y = -1850310
06 meter E =
0018531
Z = 4954529
03 I = 51
81707
XDOT = 4969
631249 Wp = 129
83913
YDOT = -5450
174371 meter/sec RA = 145
68067 deg
ZDOT = 2160
929898 TA = 299
10976
MA = 299
29517
Ha = 215
033 n
mi
Hp = 200
725
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13781124
85 X = -4203552
07
Y = -6070571
07 feet Y = -1897299
19 meter
Z = 16255016
49 Z = 4934116
01
XDOT = 16304
564464 XDOT = 5019
709519
YDOT = -17881
149511 feet/sec YDOT = -5394
320730 meter/sec
ZDOT = 7089
665020 ZDOT = 2185
194192
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11116950
22 X = 3388446
43
Y = 10289672
68 feet Y = 3136292
23 meter
Z = 16171977
31 Z = 4929218
69
XDOT = -20480
042684 XDOT = -6242
317010
YDOT = 10740
641314 feet/sec YDOT = 3273
747472 meter/sec
ZDOT = 7188
614072 ZDOT = 2191
089569
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 11242
56096291
00016717 00000-0 10270-3 0 9049
2 25544 51
6400 146
4185 0012206 133
3176 226
9000 15
60655542 37752
Satellite: ISS
Catalog Number: 25544
Epoch time: 11242
56096291 = yrday
fracday
Element set: 904
Inclination: 51
6400 deg
RA of node: 146
4185 deg
Eccentricity:
0012206
Arg of perigee: 133
3176 deg
Mean anomaly: 226
9000 deg
Mean motion: 15
60655542 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3775
Checksum: 285
Coasting Arc #6 (Orbit 3789)
---------------------------------------
Vector Time (GMT): 2011/243/12:13:08
006
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 576375
44 A = 6759889
00 meter
Y = 4574118
01 meter E =
0023697
Z = -4965358
37 I = 51
84165
XDOT = -6607
500581 Wp = 121
35524
YDOT = 3205
262135 meter/sec RA = 140
62548 deg
ZDOT = 2181
357549 TA = 169
89891
MA = 169
85120
Ha = 214
772 n
mi
Hp = 200
866
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1890995
54 X = 549304
59
Y = 15006948
86 feet Y = 4580411
65 meter
Z = -16290545
85 Z = -4962624
47
XDOT = -21678
151512 XDOT = -6653
447939
YDOT = 10515
951887 feet/sec YDOT = 3131
116288 meter/sec
ZDOT = 7156
684873 ZDOT = 2149
146656
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2792002
44 X = 851002
34
Y = -14877725
65 feet Y = -4534730
78 meter
Z = -16279565
85 Z = -4962011
67
XDOT = 22832
772985 XDOT = 6959
429206
YDOT = -3418
186786 feet/sec YDOT = -1041
863333 meter/sec
ZDOT = 7025
447910 ZDOT = 2141
356523
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 11243
52145222
00016717 00000-0 10270-3 0 9056
2 25544 51
6402 141
5825 0012066 136
8918 223
3185 15
60676426 37903
Satellite: ISS
Catalog Number: 25544
Epoch time: 11243
52145222 = yrday
fracday
Element set: 905
Inclination: 51
6402 deg
RA of node: 141
5825 deg
Eccentricity:
0012066
Arg of perigee: 136
8918 deg
Mean anomaly: 223
3185 deg
Mean motion: 15
60676426 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3790
Checksum: 293
Coasting Arc #7 (Orbit 3805)
---------------------------------------
Vector Time (GMT): 2011/244/12:13:08
006
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3020786
53 A = 6767936
09 meter
Y = -5556899
72 meter E =
0024855
Z = 2367595
86 I = 51
89080
XDOT = 5425
613708 Wp = 122
56452
YDOT = 630
748653 meter/sec RA = 135
60309 deg
ZDOT = -5414
061755 TA = 30
97709
MA = 30
83073
Ha = 214
739 n
mi
Hp = 200
935
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9910716
96 X = 3071199
03
Y = -18231298
31 feet Y = -5522837
43 meter
Z = 7767702
94 Z = 2382393
59
XDOT = 17800
569909 XDOT = 5444
457775
YDOT = 2069
385344 feet/sec YDOT = 691
526217 meter/sec
ZDOT = -17762
669801 ZDOT = -5387
658461
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14812071
26 X = -4514719
32
Y = 14500432
65 feet Y = 4419731
87 meter
Z = 7828138
69 Z = 2386016
67
XDOT = -15438
140340 XDOT = -4705
545176
YDOT = -6189
458472 feet/sec YDOT = -1886
546942 meter/sec
ZDOT = -17655
196014 ZDOT = -5381
303745
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 11244
54595813
00016717 00000-0 10270-3 0 9065
2 25544 51
6397 136
4242 0012179 140
6851 219
5192 15
60674824 38069
Satellite: ISS
Catalog Number: 25544
Epoch time: 11244
54595813 = yrday
fracday
Element set: 906
Inclination: 51
6397 deg
RA of node: 136
4242 deg
Eccentricity:
0012179
Arg of perigee: 140
6851 deg
Mean anomaly: 219
5192 deg
Mean motion: 15
60674824 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3806
Checksum: 318
Coasting Arc #8 (Orbit 3821)
---------------------------------------
Vector Time (GMT): 2011/245/12:13:08
006
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5092303
98 A = 6769397
41 meter
Y = 4224640
03 meter E =
0019221
Z = 1422945
62 I = 51
91701
XDOT = -2117
187136 Wp = 98
81231
YDOT = -4535
353425 meter/sec RA = 130
61848 deg
ZDOT = 5818
727585 TA = 276
68031
MA = 276
89904
Ha = 214
521 n
mi
Hp = 201
160
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16707034
05 X = -5146078
66
Y = 13860367
57 feet Y = 4167394
16 meter
Z = 4668456
74 Z = 1398076
46
XDOT = -6946
152022 XDOT = -2094
580860
YDOT = -14879
768456 feet/sec YDOT = -4558
902481 meter/sec
ZDOT = 19090
313600 ZDOT = 5808
497393
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19938591
08 X = 6077282
56
Y = -8638513
69 feet Y = -2633018
97 meter
Z = 4567048
40 Z = 1392036
35
XDOT = 1997
363579 XDOT = 608
796419
YDOT = 14804
476415 feet/sec YDOT = 4512
404411 meter/sec
ZDOT = 19048
823311 ZDOT = 5806
081345
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 11245
57044414
00016717 00000-0 10270-3 0 9076
2 25544 51
6397 131
2654 0011913 144
7370 215
4576 15
60724522 38225
Satellite: ISS
Catalog Number: 25544
Epoch time: 11245
57044414 = yrday
fracday
Element set: 907
Inclination: 51
6397 deg
RA of node: 131
2654 deg
Eccentricity:
0011913
Arg of perigee: 144
7370 deg
Mean anomaly: 215
4576 deg
Mean motion: 15
60724522 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3822
Checksum: 295
Coasting Arc #9 (Orbit 3836)
---------------------------------------
Vector Time (GMT): 2011/246/12:13:08
006
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4959817
20 A = 6761490
88 meter
Y = -827343
60 meter E =
0016568
Z = -4529708
39 I = 51
90961
XDOT = -1766
658977 Wp = 114
16311
YDOT = 6751
854295 meter/sec RA = 125
61121 deg
ZDOT = -3183
362422 TA = 124
09343
MA = 123
93609
Ha = 214
391 n
mi
Hp = 201
374
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16272366
14 X = 4990704
54
Y = -2714381
89 feet Y = -771707
28 meter
Z = -14861248
01 Z = -4505538
63
XDOT = -5796
125251 XDOT = -1826
564068
YDOT = 22151
752937 feet/sec YDOT = 6731
763425 meter/sec
ZDOT = -10444
102436 ZDOT = -3192
090470
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16500438
53 X = -5029333
66
Y = -1676229
84 feet Y = -510914
86 meter
Z = -14762799
31 Z = -4499701
23
XDOT = 11225
933444 XDOT = 3421
664514
YDOT = -18665
473010 feet/sec YDOT = -5689
236173 meter/sec
ZDOT = -10479
896511 ZDOT = -3194
272457
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 11246
53088410
00016717 00000-0 10270-3 0 9088
2 25544 51
6396 126
4288 0011792 148
9733 211
2122 15
60753964 38376
Satellite: ISS
Catalog Number: 25544
Epoch time: 11246
53088410 = yrday
fracday
Element set: 908
Inclination: 51
6396 deg
RA of node: 126
4288 deg
Eccentricity:
0011792
Arg of perigee: 148
9733 deg
Mean anomaly: 211
2122 deg
Mean motion: 15
60753964 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3837
Checksum: 318
Coasting Arc #10 (Orbit 3852)
---------------------------------------
Vector Time (GMT): 2011/247/12:13:08
006
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2902823
39 A = 6758344
54 meter
Y = -3138094
76 meter E =
0011986
Z = 5225981
02 I = 51
91673
XDOT = 4587
657916 Wp = 134
87865
YDOT = -6069
027201 meter/sec RA = 120
56383 deg
ZDOT = -1102
787706 TA = 325
58360
MA = 325
66117
Ha = 214
280 n
mi
Hp = 201
364
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9523698
78 X = -2892903
59
Y = -10295586
49 feet Y = -3170500
40 meter
Z = 17145607
04 Z = 5211903
30
XDOT = 15051
371114 XDOT = 4660
539111
YDOT = -19911
506565 feet/sec YDOT = -6017
317714 meter/sec
ZDOT = -3618
069901 ZDOT = -1080
323915
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6799356
66 X = 2072443
91
Y = 12346136
04 feet Y = 3763102
27 meter
Z = 17088401
16 Z = 5208544
67
XDOT = -18606
597053 XDOT = -5671
290782
YDOT = 15097
397006 feet/sec YDOT = 4601
686607 meter/sec
ZDOT = -3526
352096 ZDOT = -1074
832119
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 11247
55533648
00016717 00000-0 10270-3 0 9090
2 25544 51
6399 121
2703 0011781 152
9374 207
2399 15
60805437 38530
Satellite: ISS
Catalog Number: 25544
Epoch time: 11247
55533648 = yrday
fracday
Element set: 909
Inclination: 51
6399 deg
RA of node: 121
2703 deg
Eccentricity:
0011781
Arg of perigee: 152
9374 deg
Mean anomaly: 207
2399 deg
Mean motion: 15
60805437 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3853
Checksum: 324
Coasting Arc #11 (Orbit 3867)
---------------------------------------
Vector Time (GMT): 2011/248/12:13:08
006
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -71007
99 A = 6765607
97 meter
Y = 5968027
15 meter E =
0013480
Z = -3205309
32 I = 51
95506
XDOT = -5392
583640 Wp = 137
70379
YDOT = 2526
836081 meter/sec RA = 115
53282 deg
ZDOT = 4826
274830 TA = 185
37049
MA = 185
38497
Ha = 214
033 n
mi
Hp = 201
613
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -232965
85 X = -122167
69
Y = 19580141
57 feet Y = 5966947
03 meter
Z = -10516106
70 Z = -3205778
57
XDOT = -17692
203544 XDOT = -5443
883378
YDOT = 8290
144624 feet/sec YDOT = 2466
246105 meter/sec
ZDOT = 15834
235007 ZDOT = 4799
953286
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4653176
20 X = 1418288
11
Y = -19019434
28 feet Y = -5797123
57 meter
Z = -10518259
75 Z = -3205965
57
XDOT = 17827
242821 XDOT = 5433
743612
YDOT = -4332
202246 feet/sec YDOT = -1320
455245 meter/sec
ZDOT = 15726
932226 ZDOT = 4793
568943
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 11248
51574563
00016717 00000-0 10270-3 0 9100
2 25544 51
6394 116
4333 0011664 156
7964 203
3721 15
60803583 38689
Satellite: ISS
Catalog Number: 25544
Epoch time: 11248
51574563 = yrday
fracday
Element set: 910
Inclination: 51
6394 deg
RA of node: 116
4333 deg
Eccentricity:
0011664
Arg of perigee: 156
7964 deg
Mean anomaly: 203
3721 deg
Mean motion: 15
60803583 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3868
Checksum: 313
Coasting Arc #12 (Orbit 3883)
---------------------------------------
Vector Time (GMT): 2011/249/12:13:08
006
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2761173
68 A = 6769917
41 meter
Y = -6143223
48 meter E =
0022404
Z = -548954
47 I = 51
98140
XDOT = 4135
655299 Wp = 150
40159
YDOT = 2386
208161 meter/sec RA = 110
54889 deg
ZDOT = -6024
608407 TA = 35
51702
MA = 35
36808
Ha = 214
043 n
mi
Hp = 201
744
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9058968
78 X = 2832329
88
Y = -20154932
69 feet Y = -6111948
50 meter
Z = -1801031
71 Z = -535367
96
XDOT = 13568
422896 XDOT = 4137
930954
YDOT = 7828
766934 feet/sec YDOT = 2432
468243 meter/sec
ZDOT = -19765
775613 ZDOT = -6004
512158
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13144471
27 X = -4006434
84
Y = 17768125
00 feet Y = 5415724
50 meter
Z = -1745437
26 Z = -532009
28
XDOT = -10416
195572 XDOT = -3174
856410
YDOT = -9598
433668 feet/sec YDOT = -2925
602582 meter/sec
ZDOT = -19684
020748 ZDOT = -5999
689524
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 11249
54016524
00016717 00000-0 10270-3 0 9113
2 25544 51
6395 111
2748 0011825 160
9905 199
1694 15
60791002 38845
Satellite: ISS
Catalog Number: 25544
Epoch time: 11249
54016524 = yrday
fracday
Element set: 911
Inclination: 51
6395 deg
RA of node: 111
2748 deg
Eccentricity:
0011825
Arg of perigee: 160
9905 deg
Mean anomaly: 199
1694 deg
Mean motion: 15
60791002 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3884
Checksum: 312
Coasting Arc #13 (Orbit 3899)
---------------------------------------
Vector Time (GMT): 2011/250/12:13:08
006
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4203341
11 A = 6763227
33 meter
Y = 3497577
87 meter E =
0019135
Z = 3977973
72 I = 51
96830
XDOT = -1483
649445 Wp = 133
23575
YDOT = -6375
729711 meter/sec RA = 105
55483 deg
ZDOT = 4013
194021 TA = 275
08330
MA = 275
30169
Ha = 213
797 n
mi
Hp = 201
987
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13790489
22 X = -4261463
28
Y = 11474993
03 feet Y = 3450248
67 meter
Z = 13051094
87 Z = 3957412
95
XDOT = -4867
616289 XDOT = -1431
739577
YDOT = -20917
748396 feet/sec YDOT = -6392
030438 meter/sec
ZDOT = 13166
647049 ZDOT = 4006
112820
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15845680
97 X = 4829763
56
Y = -8541100
84 feet Y = -2603327
54 meter
Z = 12967194
23 Z = 3952400
80
XDOT = 136
988552 XDOT = 41
754111
YDOT = 20325
208826 feet/sec YDOT = 6195
123650 meter/sec
ZDOT = 13138
072197 ZDOT = 4004
484406
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 11250
56456600
00016717 00000-0 10270-3 0 9121
2 25544 51
6388 106
1149 0011517 164
5205 195
6305 15
60836018 39002
Satellite: ISS
Catalog Number: 25544
Epoch time: 11250
56456600 = yrday
fracday
Element set: 912
Inclination: 51
6388 deg
RA of node: 106
1149 deg
Eccentricity:
0011517
Arg of perigee: 164
5205 deg
Mean anomaly: 195
6305 deg
Mean motion: 15
60836018 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3900
Checksum: 287
Coasting Arc #14 (Orbit 3914)
---------------------------------------
Vector Time (GMT): 2011/251/12:13:08
006
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4068292
02 A = 6757737
91 meter
Y = 933997
93 meter E =
0020808
Z = -5329523
70 I = 51
95638
XDOT = -1514
054894 Wp = 124
07751
YDOT = 7514
193285 meter/sec RA = 100
51372 deg
ZDOT = 150
174102 TA = 147
41203
MA = 147
28344
Ha = 213
593 n
mi
Hp = 202
147
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13347414
77 X = 4083434
92
Y = 3064297
67 feet Y = 979576
49 meter
Z = -17485313
98 Z = -5309723
55
XDOT = -4967
371700 XDOT = -1598
697051
YDOT = 24652
865108 feet/sec YDOT = 7496
788944 meter/sec
ZDOT = 492
697186 ZDOT = 142
613019
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12688538
50 X = -3867466
53
Y = -5418227
77 feet Y = -1651475
82 meter
Z = -17404694
90 Z = -5304951
01
XDOT = 8900
796867 XDOT = 2712
962885
YDOT = -22442
545757 feet/sec YDOT = -6840
487947 meter/sec
ZDOT = 461
573106 ZDOT = 140
687483
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 11251
52492419
00016717 00000-0 10270-3 0 9137
2 25544 51
6376 101
2770 0011578 168
4407 191
7017 15
60894252 39156
Satellite: ISS
Catalog Number: 25544
Epoch time: 11251
52492419 = yrday
fracday
Element set: 913
Inclination: 51
6376 deg
RA of node: 101
2770 deg
Eccentricity:
0011578
Arg of perigee: 168
4407 deg
Mean anomaly: 191
7017 deg
Mean motion: 15
60894252 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3915
Checksum: 307
Coasting Arc #15 (Orbit 3930)
---------------------------------------
Vector Time (GMT): 2011/252/12:13:08
006
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2512679
37 A = 6763423
42 meter
Y = -4978959
37 meter E =
0016164
Z = 3807031
80 I = 51
98095
XDOT = 3817
483065 Wp = 127
77429
YDOT = -5162
977459 meter/sec RA = 95
47685 deg
ZDOT = -4230
228748 TA = 6
52949
MA = 6
50845
Ha = 213
394 n
mi
Hp = 202
229
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8243698
73 X = -2475310
49
Y = -16335168
53 feet Y = -5006848
49 meter
Z = 12490261
80 Z = 3794916
51
XDOT = 12524
550738 XDOT = 3895
482103
YDOT = -16938
902426 feet/sec YDOT = -5119
852194 meter/sec
ZDOT = -13878
703240 ZDOT = -4211
493934
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5567050
71 X = 1696837
05
Y = 17465089
34 feet Y = 5323359
23 meter
Z = 12441122
95 Z = 3792054
28
XDOT = -13908
450695 XDOT = -4239
295772
YDOT = 14271
094194 feet/sec YDOT = 4349
829510 meter/sec
ZDOT = -13802
155936 ZDOT = -4206
897129
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 11252
54928868
00016717 00000-0 10270-3 0 9143
2 25544 51
6381 96
1181 0011442 173
1887 186
9426 15
60943213 39315
Satellite: ISS
Catalog Number: 25544
Epoch time: 11252
54928868 = yrday
fracday
Element set: 914
Inclination: 51
6381 deg
RA of node: 96
1181 deg
Eccentricity:
0011442
Arg of perigee: 173
1887 deg
Mean anomaly: 186
9426 deg
Mean motion: 15
60943213 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3931
Checksum: 322
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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