[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
September 29th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 27447 97 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
278/21:17:39
498 -2
1 7
8 7
8
N/A -4
7 -0
3 211
2
000/00:25:18
995 -5
9 -0
1 207
1
Coasting Arc #1 (Orbit 1704)
---------------------------------------
Vector Time (GMT): 2011/271/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6190524
60 A = 6765410
98 meter
Y = 1700570
25 meter E =
0003345
Z = 2130585
37 I = 51
65840
XDOT = -3095
930961 Wp = 80
28844
YDOT = 4353
378029 meter/sec RA =
14269 deg
ZDOT = 5513
841559 TA = 303
38947
MA = 303
42147
Ha = 208
541 n
mi
Hp = 205
376
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20310120
08 X = 6160698
26
Y = 5579298
73 feet Y = 1769629
96 meter
Z = 6990109
48 Z = 2160586
69
XDOT = -10157
253810 XDOT = -3171
166787
YDOT = 14282
736315 feet/sec YDOT = 4318
337375 meter/sec
ZDOT = 18090
031361 ZDOT = 5498
618103
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20747262
43 X = -6323765
59
Y = -3385129
32 feet Y = -1031787
42 meter
Z = 7112185
56 Z = 2167794
16
XDOT = 8436
561227 XDOT = 2571
463862
YDOT = -13784
584032 feet/sec YDOT = -4201
541213 meter/sec
ZDOT = 18027
771755 ZDOT = 5494
864831
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 11271
55970087
00016717 00000-0 10270-3 0 9000
2 25544 51
6421
3401 0010677 247
7284 112
2741 15
61695662 17052
Satellite: ISS
Catalog Number: 25544
Epoch time: 11271
55970087 = yrday
fracday
Element set: 900
Inclination: 51
6421 deg
RA of node:
3401 deg
Eccentricity:
0010677
Arg of perigee: 247
7284 deg
Mean anomaly: 112
2741 deg
Mean motion: 15
61695662 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1705
Checksum: 286
Coasting Arc #2 (Orbit 1719)
---------------------------------------
Vector Time (GMT): 2011/272/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2677042
13 A = 6756685
51 meter
Y = -3720932
14 meter E =
0002135
Z = -4965811
32 I = 51
59840
XDOT = 7031
995407 Wp = 89
16348
YDOT = -2267
721441 meter/sec RA = 355
09803 deg
ZDOT = -2092
429513 TA = 160
49416
MA = 160
48599
Ha = 208
130 n
mi
Hp = 205
495
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8782946
63 X = -2611111
59
Y = -12207782
60 feet Y = -3750500
24 meter
Z = -16292031
90 Z = -4978656
13
XDOT = 23070
851072 XDOT = 7066
995674
YDOT = -7440
030973 feet/sec YDOT = -2188
889840 meter/sec
ZDOT = -6864
926225 ZDOT = -2058
182358
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10129070
85 X = 3087340
80
Y = 11039582
11 feet Y = 3364864
63 meter
Z = -16344110
92 Z = -4981685
01
XDOT = -21207
977516 XDOT = -6464
191547
YDOT = 9505
567076 feet/sec YDOT = 2897
296845 meter/sec
ZDOT = -6725
324086 ZDOT = -2049
878782
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 11272
51953863
00016717 00000-0 10270-3 0 9011
2 25544 51
6414 355
5011 0010711 252
0077 107
9913 15
61732516 17203
Satellite: ISS
Catalog Number: 25544
Epoch time: 11272
51953863 = yrday
fracday
Element set: 901
Inclination: 51
6414 deg
RA of node: 355
5011 deg
Eccentricity:
0010711
Arg of perigee: 252
0077 deg
Mean anomaly: 107
9913 deg
Mean motion: 15
61732516 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1720
Checksum: 278
Coasting Arc #3 (Orbit 1735)
---------------------------------------
Vector Time (GMT): 2011/273/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2238889
20 A = 6757331
30 meter
Y = 4235877
28 meter E =
0003826
Z = 4768732
03 I = 51
57140
XDOT = -7168
539333 Wp = 287
23290
YDOT = -845
067934 meter/sec RA = 350
01524 deg
ZDOT = -2615
561466 TA = 188
54177
MA = 188
54828
Ha = 207
621 n
mi
Hp = 205
500
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7345437
01 X = -2309255
19
Y = 13897235
17 feet Y = 4210447
48 meter
Z = 15645446
29 Z = 4757684
18
XDOT = -23518
829833 XDOT = -7145
850720
YDOT = -2772
532591 feet/sec YDOT = -925
104219 meter/sec
ZDOT = -8581
238405 ZDOT = -2650
331572
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5408057
07 X = 1648375
80
Y = -14807276
64 feet Y = -4513257
92 meter
Z = 15600194
13 Z = 4754939
17
XDOT = 22543
525145 XDOT = 6871
266464
YDOT = -954
162383 feet/sec YDOT = -290
828694 meter/sec
ZDOT = -8722
774524 ZDOT = -2658
701675
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 11273
54332523
00016717 00000-0 10270-3 0 9020
2 25544 51
6417 350
3380 0010597 256
8406 103
1568 15
61838732 17366
Satellite: ISS
Catalog Number: 25544
Epoch time: 11273
54332523 = yrday
fracday
Element set: 902
Inclination: 51
6417 deg
RA of node: 350
3380 deg
Eccentricity:
0010597
Arg of perigee: 256
8406 deg
Mean anomaly: 103
1568 deg
Mean motion: 15
61838732 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1736
Checksum: 300
Coasting Arc #4 (Orbit 1750)
---------------------------------------
Vector Time (GMT): 2011/274/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5885566
51 A = 6765949
73 meter
Y = -2909225
41 meter E =
0007295
Z = -1617878
32 I = 51
56971
XDOT = 3446
754270 Wp = 310
90090
YDOT = 3780
678952 meter/sec RA = 344
97249 deg
ZDOT = 5728
227669 TA = 31
31456
MA = 31
27113
Ha = 207
109 n
mi
Hp = 205
451
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19309601
42 X = 5925520
06
Y = -9544702
80 feet Y = -2843186
08 meter
Z = -5307999
74 Z = -1589188
75
XDOT = 11308
248918 XDOT = 3376
394784
YDOT = 12403
802335 feet/sec YDOT = 3818
829487 meter/sec
ZDOT = 18793
397864 ZDOT = 5744
801143
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17592084
61 X = -5362067
39
Y = 12478345
47 feet Y = 3803399
70 meter
Z = -5190989
62 Z = -1582213
64
XDOT = -12102
531311 XDOT = -3688
851543
YDOT = -9199
256484 feet/sec YDOT = -2803
933376 meter/sec
ZDOT = 18860
648933 ZDOT = 5748
725795
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 11274
50309000
00016717 00000-0 10270-3 0 9032
2 25544 51
6408 345
4977 0010505 261
4470 98
5496 15
61834011 17515
Satellite: ISS
Catalog Number: 25544
Epoch time: 11274
50309000 = yrday
fracday
Element set: 903
Inclination: 51
6408 deg
RA of node: 345
4977 deg
Eccentricity:
0010505
Arg of perigee: 261
4470 deg
Mean anomaly: 98
5496 deg
Mean motion: 15
61834011 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1751
Checksum: 291
Coasting Arc #5 (Orbit 1766)
---------------------------------------
Vector Time (GMT): 2011/275/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6259831
54 A = 6763904
16 meter
Y = 129540
06 meter E =
0007466
Z = -2547087
14 I = 51
53412
XDOT = 2040
069474 Wp = 236
47172
YDOT = -5201
973177 meter/sec RA = 339
95834 deg
ZDOT = -5271
254410 TA = 332
29628
MA = 332
33604
Ha = 206
467 n
mi
Hp = 205
171
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20537505
06 X = -6248441
45
Y = 425000
18 feet Y = 59602
39 meter
Z = -8356585
12 Z = -2577469
97
XDOT = 6693
141320 XDOT = 2123
694336
YDOT = -17066
841133 feet/sec YDOT = -5178
692463 meter/sec
ZDOT = -17294
141765 ZDOT = -5261
140389
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20097042
25 X = 6125578
48
Y = -3999423
30 feet Y = -1219024
22 meter
Z = -8480316
04 Z = -2584800
33
XDOT = -4000
618326 XDOT = -1219
388466
YDOT = 16527
634747 feet/sec YDOT = 5037
623071 meter/sec
ZDOT = -17252
627812 ZDOT = -5258
600957
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 11275
52679979
00016717 00000-0 10270-3 0 9041
2 25544 51
6401 340
3343 0010323 264
9020 95
0959 15
61923267 17671
Satellite: ISS
Catalog Number: 25544
Epoch time: 11275
52679979 = yrday
fracday
Element set: 904
Inclination: 51
6401 deg
RA of node: 340
3343 deg
Eccentricity:
0010323
Arg of perigee: 264
9020 deg
Mean anomaly: 95
0959 deg
Mean motion: 15
61923267 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1767
Checksum: 316
Coasting Arc #6 (Orbit 1782)
---------------------------------------
Vector Time (GMT): 2011/276/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3250977
60 A = 6755224
47 meter
Y = 2980497
24 meter E =
0007160
Z = 5123024
93 I = 51
47799
XDOT = -6229
615986 Wp = 246
50320
YDOT = 4229
777507 meter/sec RA = 334
89506 deg
ZDOT = 1491
230901 TA = 189
11287
MA = 189
12587
Ha = 206
131 n
mi
Hp = 204
804
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10665937
02 X = 3192520
65
Y = 9778534
25 feet Y = 3016524
98 meter
Z = 16807824
57 Z = 5138676
14
XDOT = -20438
372658 XDOT = -6283
695345
YDOT = 13877
222793 feet/sec YDOT = 4159
811804 meter/sec
ZDOT = 4892
489834 ZDOT = 1460
835810
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12243332
46 X = -3731767
73
Y = -7572486
01 feet Y = -2308093
74 meter
Z = 16871371
52 Z = 5142394
04
XDOT = 16874
961630 XDOT = 5143
488305
YDOT = -16651
345242 feet/sec YDOT = -5075
330030 meter/sec
ZDOT = 4768
450507 ZDOT = 1453
423714
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 11276
55046736
00016717 00000-0 10270-3 0 9055
2 25544 51
6406 335
1702 0010344 269
3435 90
6536 15
62001502 17839
Satellite: ISS
Catalog Number: 25544
Epoch time: 11276
55046736 = yrday
fracday
Element set: 905
Inclination: 51
6406 deg
RA of node: 335
1702 deg
Eccentricity:
0010344
Arg of perigee: 269
3435 deg
Mean anomaly: 90
6536 deg
Mean motion: 15
62001502 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1783
Checksum: 288
Coasting Arc #7 (Orbit 1797)
---------------------------------------
Vector Time (GMT): 2011/277/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1371349
00 A = 6757912
30 meter
Y = -4898612
27 meter E =
0002932
Z = -4449196
89 I = 51
45983
XDOT = 6886
838083 Wp = 206
28695
YDOT = -1019
715426 meter/sec RA = 329
80338 deg
ZDOT = 3242
006722 TA = 96
39389
MA = 96
36050
Ha = 206
181 n
mi
Hp = 205
031
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4499176
52 X = 1447637
74
Y = -16071562
57 feet Y = -4882850
65 meter
Z = -14597102
66 Z = -4442349
35
XDOT = 22594
613134 XDOT = 6881
979797
YDOT = -3345
523051 feet/sec YDOT = -942
729606 meter/sec
ZDOT = 10636
504994 ZDOT = 3275
451248
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1133913
42 X = -345616
81
Y = 16675554
05 feet Y = 5082708
87 meter
Z = -14568914
04 Z = -4440605
00
XDOT = -20120
813669 XDOT = -6132
824006
YDOT = 8053
401658 feet/sec YDOT = 2454
676825 meter/sec
ZDOT = 10772
760028 ZDOT = 3283
537257
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 11277
51012044
00016717 00000-0 10270-3 0 9068
2 25544 51
6400 330
3288 0010104 273
8424 86
1577 15
62063698 17986
Satellite: ISS
Catalog Number: 25544
Epoch time: 11277
51012044 = yrday
fracday
Element set: 906
Inclination: 51
6400 deg
RA of node: 330
3288 deg
Eccentricity:
0010104
Arg of perigee: 273
8424 deg
Mean anomaly: 86
1577 deg
Mean motion: 15
62063698 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1798
Checksum: 298
Coasting Arc #8 (Orbit 1813)
---------------------------------------
Vector Time (GMT): 2011/278/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5012403
60 A = 6765811
76 meter
Y = 4442786
76 meter E =
0006426
Z = 924584
04 I = 51
46193
XDOT = -3815
162552 Wp = 170
36613
YDOT = -3073
378846 meter/sec RA = 324
76008 deg
ZDOT = -5915
114470 TA = 359
56569
MA = 359
56624
Ha = 206
629 n
mi
Hp = 205
173
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16444893
69 X = -5066202
63
Y = 14576072
04 feet Y = 4386434
24 meter
Z = 3033412
21 Z = 900102
87
XDOT = -12516
937508 XDOT = -3751
777345
YDOT = -10083
263931 feet/sec YDOT = -3115
688279 meter/sec
ZDOT = -19406
543537 ZDOT = -5933
494361
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12754296
49 X = 3887509
57
Y = -17911470
82 feet Y = -5459416
30 meter
Z = 2933449
92 Z = 894115
54
XDOT = 13047
207263 XDOT = 3976
788774
YDOT = 6100
199346 feet/sec YDOT = 1859
340761 meter/sec
ZDOT = -19481
201214 ZDOT = -5937
870130
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 11278
53370976
00016717 00000-0 10270-3 0 9073
2 25544 51
6406 325
1645 0010088 278
6221 81
3792 15
62135141 18148
Satellite: ISS
Catalog Number: 25544
Epoch time: 11278
53370976 = yrday
fracday
Element set: 907
Inclination: 51
6406 deg
RA of node: 325
1645 deg
Eccentricity:
0010088
Arg of perigee: 278
6221 deg
Mean anomaly: 81
3792 deg
Mean motion: 15
62135141 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1814
Checksum: 305
Coasting Arc #9 (Orbit 1819)
---------------------------------------
Vector Time (GMT): 2011/278/21:30:18
995
Vector Time (MET): N/A
Weight (LBS) : 870439
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4978221
21 A = 6762897
66 meter
Y = -741205
87 meter E =
0002504
Z = -4514692
59 I = 51
42418
XDOT = 3717
101802 Wp = 225
05503
YDOT = -5949
838680 meter/sec RA = 322
78873 deg
ZDOT = -3122
595304 TA = 13
60666
MA = 13
59991
Ha = 211
198 n
mi
Hp = 207
097
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16332746
75 X = -4947631
37
Y = -2431777
80 feet Y = -796704
66 meter
Z = -14811983
55 Z = -4538802
40
XDOT = 12195
215886 XDOT = 3798
526786
YDOT = -19520
468111 feet/sec YDOT = -5907
816708 meter/sec
ZDOT = -10244
735249 ZDOT = -3104
339471
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13848528
29 X = -4221031
42
Y = -8830271
86 feet Y = -2691466
86 meter
Z = -14910116
67 Z = -4544603
56
XDOT = 18494
416063 XDOT = 5637
098016
YDOT = -11836
211166 feet/sec YDOT = -3607
677164 meter/sec
ZDOT = -10170
034438 ZDOT = -3099
826497
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 11278
91758153
00016717 00000-0 10270-3 0 9083
2 25544 51
6410 323
2290 0012283 244
9938 114
9942 15
60201691 18207
Satellite: ISS
Catalog Number: 25544
Epoch time: 11278
91758153 = yrday
fracday
Element set: 908
Inclination: 51
6410 deg
RA of node: 323
2290 deg
Eccentricity:
0012283
Arg of perigee: 244
9938 deg
Mean anomaly: 114
9942 deg
Mean motion: 15
60201691 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1820
Checksum: 304
Coasting Arc #10 (Orbit 1835)
---------------------------------------
Vector Time (GMT): 2011/279/21:30:18
995
Vector Time (MET): N/A
Weight (LBS) : 870439
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2012190
33 A = 6759838
90 meter
Y = 3804393
52 meter E =
0008883
Z = 5219773
48 I = 51
39062
XDOT = -6115
499228 Wp = 253
03755
YDOT = 4535
067584 meter/sec RA = 317
71137 deg
ZDOT = -951
749261 TA = 206
07379
MA = 206
11856
Ha = 210
847 n
mi
Hp = 206
966
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6601674
31 X = 1944142
60
Y = 12481606
02 feet Y = 3826515
03 meter
Z = 17125241
08 Z = 5229383
08
XDOT = -20063
973845 XDOT = -6161
133302
YDOT = 14878
830656 feet/sec YDOT = 4466
425091 meter/sec
ZDOT = -3122
536945 ZDOT = -981
569556
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1099447
17 X = 335111
50
Y = 14029604
21 feet Y = 4276223
36 meter
Z = 17164145
66 Z = 5231631
60
XDOT = -23243
881633 XDOT = -7084
735122
YDOT = 5775
047943 feet/sec YDOT = 1760
234613 meter/sec
ZDOT = -3244
235653 ZDOT = -988
843027
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 11279
94239792
00016717 00000-0 10270-3 0 9091
2 25544 51
6406 318
0729 0012372 249
0914 110
8918 15
60274015 18365
Satellite: ISS
Catalog Number: 25544
Epoch time: 11279
94239792 = yrday
fracday
Element set: 909
Inclination: 51
6406 deg
RA of node: 318
0729 deg
Eccentricity:
0012372
Arg of perigee: 249
0914 deg
Mean anomaly: 110
8918 deg
Mean motion: 15
60274015 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1836
Checksum: 320
Coasting Arc #11 (Orbit 1850)
---------------------------------------
Vector Time (GMT): 2011/280/21:30:18
995
Vector Time (MET): N/A
Weight (LBS) : 870439
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1511556
00 A = 6766532
75 meter
Y = -5649814
67 meter E =
0007734
Z = -3400854
30 I = 51
39180
XDOT = 6044
209867 Wp = 242
10482
YDOT = -1152
637931 meter/sec RA = 312
64525 deg
ZDOT = 4589
755337 TA = 77
85812
MA = 77
77148
Ha = 210
541 n
mi
Hp = 207
076
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4959173
24 X = 1591141
76
Y = -18536137
37 feet Y = -5632466
88 meter
Z = -11157658
46 Z = -3393317
27
XDOT = 19830
084867 XDOT = 6034
353432
YDOT = -3781
620508 feet/sec YDOT = -1085
102525 meter/sec
ZDOT = 15058
252417 ZDOT = 4619
094320
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11613584
92 X = 3539820
68
Y = -15296982
30 feet Y = -4662520
20 meter
Z = -11126639
57 Z = -3391399
74
XDOT = 18600
096541 XDOT = 5669
309426
YDOT = 3053
767728 feet/sec YDOT = 930
788403 meter/sec
ZDOT = 15177
785064 ZDOT = 4626
188888
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 11280
90313080
00016717 00000-0 10270-3 0 9104
2 25544 51
6408 313
2385 0012252 252
8100 107
1715 15
60300795 18514
Satellite: ISS
Catalog Number: 25544
Epoch time: 11280
90313080 = yrday
fracday
Element set: 910
Inclination: 51
6408 deg
RA of node: 313
2385 deg
Eccentricity:
0012252
Arg of perigee: 252
8100 deg
Mean anomaly: 107
1715 deg
Mean motion: 15
60300795 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1851
Checksum: 262
Coasting Arc #12 (Orbit 1866)
---------------------------------------
Vector Time (GMT): 2011/281/21:30:18
995
Vector Time (MET): N/A
Weight (LBS) : 870439
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4175052
69 A = 6771407
42 meter
Y = 5320628
26 meter E =
0012058
Z = -73828
52 I = 51
38839
XDOT = -3729
245709 Wp = 196
58374
YDOT = -3012
783029 meter/sec RA = 307
62147 deg
ZDOT = -6001
491771 TA = 344
21668
MA = 344
25423
Ha = 210
235 n
mi
Hp = 207
016
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13697679
42 X = -4233880
05
Y = 17456129
46 feet Y = 5273611
33 meter
Z = -242219
57 Z = -94254
51
XDOT = -12235
058102 XDOT = -3666
124700
YDOT = -9884
458758 feet/sec YDOT = -3054
133474 meter/sec
ZDOT = -19689
933632 ZDOT = -6019
454879
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19051727
01 X = -5806966
39
Y = 11372210
42 feet Y = 3466249
74 meter
Z = -325692
93 Z = -99271
21
XDOT = -6927
820198 XDOT = -2111
599596
YDOT = -12188
200262 feet/sec YDOT = -3714
963440 meter/sec
ZDOT = -19762
902959 ZDOT = -6023
732822
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 11281
92787568
00016717 00000-0 10270-3 0 9114
2 25544 51
6406 308
0822 0012270 255
8450 104
1343 15
60313983 18675
Satellite: ISS
Catalog Number: 25544
Epoch time: 11281
92787568 = yrday
fracday
Element set: 911
Inclination: 51
6406 deg
RA of node: 308
0822 deg
Eccentricity:
0012270
Arg of perigee: 255
8450 deg
Mean anomaly: 104
1343 deg
Mean motion: 15
60313983 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1867
Checksum: 303
Coasting Arc #13 (Orbit 1882)
---------------------------------------
Vector Time (GMT): 2011/282/21:30:18
995
Vector Time (MET): N/A
Weight (LBS) : 870439
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5091373
10 A = 6765750
60 meter
Y = -2714732
04 meter E =
0002569
Z = 3535552
34 I = 51
35230
XDOT = 234
852666 Wp = 176
88194
YDOT = 6244
863492 meter/sec RA = 302
59321 deg
ZDOT = 4454
171136 TA = 225
10621
MA = 225
12707
Ha = 209
712 n
mi
Hp = 206
815
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16703979
99 X = 5104176
13
Y = -8906601
18 feet Y = -2657725
20 meter
Z = 11599581
16 Z = 3560317
86
XDOT = 770
513995 XDOT = 143
366162
YDOT = 20488
397283 feet/sec YDOT = 6246
978739 meter/sec
ZDOT = 14613
422362 ZDOT = 4455
089123
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18679561
67 X = 5693530
40
Y = -2659217
80 feet Y = -810529
58 meter
Z = 11700568
87 Z = 3566333
39
XDOT = -6581
950900 XDOT = -2006
178634
YDOT = 18117
651476 feet/sec YDOT = 5522
260170 meter/sec
ZDOT = 14616
809364 ZDOT = 4455
203494
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 11282
95258090
00016717 00000-0 10270-3 0 9122
2 25544 51
6403 302
9244 0012112 260
9655 99
0130 15
60392457 18839
Satellite: ISS
Catalog Number: 25544
Epoch time: 11282
95258090 = yrday
fracday
Element set: 912
Inclination: 51
6403 deg
RA of node: 302
9244 deg
Eccentricity:
0012112
Arg of perigee: 260
9655 deg
Mean anomaly: 99
0130 deg
Mean motion: 15
60392457 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1883
Checksum: 295
Coasting Arc #14 (Orbit 1897)
---------------------------------------
Vector Time (GMT): 2011/283/21:30:18
995
Vector Time (MET): N/A
Weight (LBS) : 870439
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4083980
20 A = 6759032
27 meter
Y = -1245418
87 meter E =
0002506
Z = -5241892
27 I = 51
31468
XDOT = 3030
890358 Wp = 85
76516
YDOT = -7019
688249 meter/sec RA = 297
51917 deg
ZDOT = -693
679154 TA = 177
58861
MA = 177
58740
Ha = 209
186 n
mi
Hp = 206
645
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13398885
16 X = -4044285
64
Y = -4086019
92 feet Y = -1290867
08 meter
Z = -17197809
27 Z = -5261635
94
XDOT = 9943
866003 XDOT = 3112
530440
YDOT = -23030
473257 feet/sec YDOT = -6985
338578 meter/sec
ZDOT = -2275
850243 ZDOT = -678
755806
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11228892
25 X = -3422566
36
Y = -8207842
10 feet Y = -2501750
27 meter
Z = -17278125
85 Z = -5266372
76
XDOT = 16339
552137 XDOT = 4980
295491
YDOT = -17692
234936 feet/sec YDOT = -5392
593209 meter/sec
ZDOT = -2214
701540 ZDOT = -675
041029
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 11283
91320548
00016717 00000-0 10270-3 0 9138
2 25544 51
6397 298
0892 0012196 264
5968 95
3797 15
60491847 18981
Satellite: ISS
Catalog Number: 25544
Epoch time: 11283
91320548 = yrday
fracday
Element set: 913
Inclination: 51
6397 deg
RA of node: 298
0892 deg
Eccentricity:
0012196
Arg of perigee: 264
5968 deg
Mean anomaly: 95
3797 deg
Mean motion: 15
60491847 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1898
Checksum: 363
Coasting Arc #15 (Orbit 1913)
---------------------------------------
Vector Time (GMT): 2011/284/21:30:18
995
Vector Time (MET): N/A
Weight (LBS) : 870439
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1728182
91 A = 6762618
72 meter
Y = 4901717
41 meter E =
0004167
Z = 4330986
05 I = 51
31454
XDOT = -4938
673425 Wp = 311
36494
YDOT = 4770
162713 meter/sec RA = 292
43382 deg
ZDOT = -3427
538980 TA = 173
53972
MA = 173
53435
Ha = 209
052 n
mi
Hp = 206
382
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5669891
43 X = 1652202
99
Y = 16081750
03 feet Y = 4920618
63 meter
Z = 14209271
81 Z = 4339196
64
XDOT = -16202
996800 XDOT = -4974
996615
YDOT = 15650
140134 feet/sec YDOT = 4714
731992 meter/sec
ZDOT = -11245
206626 ZDOT = -3451
620182
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 313647
15 X = 95599
65
Y = 17021414
07 feet Y = 5188127
01 meter
Z = 14242431
19 Z = 4341093
03
XDOT = -18955
825341 XDOT = -5777
735564
YDOT = 9842
356816 feet/sec YDOT = 2999
950358 meter/sec
ZDOT = -11343
511279 ZDOT = -3457
502238
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 11284
93783403
00016717 00000-0 10270-3 0 9145
2 25544 51
6399 292
9318 0012254 268
6994 91
2758 15
60570208 19148
Satellite: ISS
Catalog Number: 25544
Epoch time: 11284
93783403 = yrday
fracday
Element set: 914
Inclination: 51
6399 deg
RA of node: 292
9318 deg
Eccentricity:
0012254
Arg of perigee: 268
6994 deg
Mean anomaly: 91
2758 deg
Mean motion: 15
60570208 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1914
Checksum: 337
Coasting Arc #16 (Orbit 1928)
---------------------------------------
Vector Time (GMT): 2011/285/21:30:18
995
Vector Time (MET): N/A
Weight (LBS) : 870439
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1043580
51 A = 6770009
53 meter
Y = -6572502
57 meter E =
0010120
Z = -1209869
11 I = 51
32798
XDOT = 4984
242292 Wp = 319
43184
YDOT = -286
560094 meter/sec RA = 287
38867 deg
ZDOT = 5835
975734 TA = 27
32374
MA = 27
27055
Ha = 209
020 n
mi
Hp = 206
435
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3423820
57 X = 1122875
41
Y = -21563328
64 feet Y = -6560389
36 meter
Z = -3969386
83 Z = -1204606
09
XDOT = 16352
500957 XDOT = 4958
725539
YDOT = -940
157790 feet/sec YDOT = -230
965388 meter/sec
ZDOT = 19146
902014 ZDOT = 5860
127703
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9638066
87 X = 2937682
78
Y = -19595403
25 feet Y = -5972678
91 meter
Z = -3947601
77 Z = -1203229
02
XDOT = 14365
728589 XDOT = 4378
674074
YDOT = 3175
529443 feet/sec YDOT = 967
901374 meter/sec
ZDOT = 19245
247484 ZDOT = 5865
951433
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 11285
89838845
00016717 00000-0 10270-3 0 9153
2 25544 51
6390 288
0952 0012204 272
0660 87
9098 15
60584238 19296
Satellite: ISS
Catalog Number: 25544
Epoch time: 11285
89838845 = yrday
fracday
Element set: 915
Inclination: 51
6390 deg
RA of node: 288
0952 deg
Eccentricity:
0012204
Arg of perigee: 272
0660 deg
Mean anomaly: 87
9098 deg
Mean motion: 15
60584238 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1929
Checksum: 343
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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