[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
June 24th 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) : 102 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 186 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
180/12:36:15
446 6
6 8
5 8
6
N/A -0
6 -1
7 211
0
000/00:32:30
893 -5
5 -0
0 209
3
Coasting Arc #1 (Orbit 174)
---------------------------------------
Vector Time (GMT): 2011/173/13:48:14
468
Vector Time (MET): N/A
Weight (LBS) : 883811
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 505770
00 A = 6756954
84 meter
Y = 4861031
33 meter E =
0002515
Z = -4665682
08 I = 51
88000
XDOT = -6233
737216 Wp = 214
66788
YDOT = 3429
102172 meter/sec RA = 132
57135 deg
ZDOT = 2894
144344 TA = 83
96366
MA = 83
93500
Ha = 206
824 n
mi
Hp = 204
441
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1659350
38 X = 474040
29
Y = 15948265
53 feet Y = 4866510
24 meter
Z = -15307355
92 Z = -4663301
63
XDOT = -20451
893754 XDOT = -6285
677920
YDOT = 11250
335211 feet/sec YDOT = 3359
102011 meter/sec
ZDOT = 9495
224227 ZDOT = 2863
735261
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13464794
26 X = 4104069
29
Y = -8722937
94 feet Y = -2658751
48 meter
Z = -15297889
77 Z = -4662796
80
XDOT = 18622
926486 XDOT = 5676
267993
YDOT = 12294
851218 feet/sec YDOT = 3747
470651 meter/sec
ZDOT = 9371
681509 ZDOT = 2856
488524
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 11173
58612512
00016717 00000-0 10270-3 0 9000
2 25544 51
6399 133
5106 0011610 277
4574 82
5263 15
62093923 1758
Satellite: ISS
Catalog Number: 25544
Epoch time: 11173
58612512 = yrday
fracday
Element set: 900
Inclination: 51
6399 deg
RA of node: 133
5106 deg
Eccentricity:
0011610
Arg of perigee: 277
4574 deg
Mean anomaly: 82
5263 deg
Mean motion: 15
62093923 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 175
Checksum: 292
Coasting Arc #2 (Orbit 190)
---------------------------------------
Vector Time (GMT): 2011/174/13:48:14
468
Vector Time (MET): N/A
Weight (LBS) : 883811
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3193180
39 A = 6765477
05 meter
Y = -5818321
81 meter E =
0004839
Z = 1295569
08 I = 51
92893
XDOT = 4780
168770 Wp = 173
39491
YDOT = 1318
265869 meter/sec RA = 127
55372 deg
ZDOT = -5863
921923 TA = 352
51980
MA = 352
52702
Ha = 207
050 n
mi
Hp = 204
519
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10476313
60 X = 3251711
04
Y = -19088982
31 feet Y = -5782286
60 meter
Z = 4250554
71 Z = 1311223
03
XDOT = 15682
968405 XDOT = 4793
558152
YDOT = 4325
019255 feet/sec YDOT = 1371
796118 meter/sec
ZDOT = -19238
588987 ZDOT = -5840
667286
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21758652
15 X = -6632037
18
Y = -396571
80 feet Y = -120875
09 meter
Z = 4314324
41 Z = 1315006
08
XDOT = -3531
620182 XDOT = -1076
437831
YDOT = -14413
733430 feet/sec YDOT = -4393
305950 meter/sec
ZDOT = -19144
265344 ZDOT = -5835
172077
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 11174
60969932
00016717 00000-0 10270-3 0 9016
2 25544 51
6404 128
3466 0011580 281
2260 78
7595 15
62112835 1914
Satellite: ISS
Catalog Number: 25544
Epoch time: 11174
60969932 = yrday
fracday
Element set: 901
Inclination: 51
6404 deg
RA of node: 128
3466 deg
Eccentricity:
0011580
Arg of perigee: 281
2260 deg
Mean anomaly: 78
7595 deg
Mean motion: 15
62112835 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 191
Checksum: 304
Coasting Arc #3 (Orbit 206)
---------------------------------------
Vector Time (GMT): 2011/175/13:48:14
468
Vector Time (MET): N/A
Weight (LBS) : 883811
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4969932
96 A = 6762552
97 meter
Y = 3523529
64 meter E =
0005355
Z = 2927223
67 I = 51
93659
XDOT = -1059
718999 Wp = 21
90013
YDOT = -5689
349564 meter/sec RA = 122
56283 deg
ZDOT = 5050
992915 TA = 11
47161
MA = 11
45941
Ha = 207
492 n
mi
Hp = 204
559
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16305554
32 X = -5023184
27
Y = 11560136
60 feet Y = 3467654
74 meter
Z = 9603752
18 Z = 2902950
81
XDOT = -3476
768369 XDOT = -1020
557617
YDOT = -18665
845027 feet/sec YDOT = -5700
981611 meter/sec
ZDOT = 16571
499064 ZDOT = 5045
939265
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17989130
94 X = 5483087
11
Y = 8819547
63 feet Y = 2688198
12 meter
Z = 9505086
18 Z = 2897150
27
XDOT = -14023
897498 XDOT = -4274
483957
YDOT = 10773
381676 feet/sec YDOT = 3283
726735 meter/sec
ZDOT = 16551
229529 ZDOT = 5044
814760
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 11175
63325550
00016717 00000-0 10270-3 0 9023
2 25544 51
6401 123
1817 0011613 285
2977 74
6896 15
62137257 2072
Satellite: ISS
Catalog Number: 25544
Epoch time: 11175
63325550 = yrday
fracday
Element set: 902
Inclination: 51
6401 deg
RA of node: 123
1817 deg
Eccentricity:
0011613
Arg of perigee: 285
2977 deg
Mean anomaly: 74
6896 deg
Mean motion: 15
62137257 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 207
Checksum: 299
Coasting Arc #4 (Orbit 221)
---------------------------------------
Vector Time (GMT): 2011/176/13:48:14
468
Vector Time (MET): N/A
Weight (LBS) : 883811
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4147639
53 A = 6754302
38 meter
Y = 941470
22 meter E =
0006570
Z = -5250702
13 I = 51
92549
XDOT = -2832
695517 Wp = 30
83260
YDOT = 7071
760563 meter/sec RA = 117
52220 deg
ZDOT = -964
640451 TA = 229
95602
MA = 230
01368
Ha = 207
683 n
mi
Hp = 204
412
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13607741
24 X = 4162310
55
Y = 3088813
07 feet Y = 987934
36 meter
Z = -17226713
04 Z = -5230517
12
XDOT = -9293
620461 XDOT = -2906
876721
YDOT = 23201
314182 feet/sec YDOT = 7039
668995 meter/sec
ZDOT = -3164
830875 ZDOT = -978
580972
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4093684
03 X = -1247754
89
Y = -13444990
91 feet Y = -4098033
23 meter
Z = -17144824
31 Z = -5225742
45
XDOT = 23772
320511 XDOT = 7245
803292
YDOT = -3108
919308 feet/sec YDOT = -947
598605 meter/sec
ZDOT = -3221
727402 ZDOT = -981
982512
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 11176
59282266
00016717 00000-0 10270-3 0 9036
2 25544 51
6408 118
3399 0011597 288
9269 71
0631 15
62188325 2222
Satellite: ISS
Catalog Number: 25544
Epoch time: 11176
59282266 = yrday
fracday
Element set: 903
Inclination: 51
6408 deg
RA of node: 118
3399 deg
Eccentricity:
0011597
Arg of perigee: 288
9269 deg
Mean anomaly: 71
0631 deg
Mean motion: 15
62188325 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 222
Checksum: 322
Coasting Arc #5 (Orbit 237)
---------------------------------------
Vector Time (GMT): 2011/177/13:48:14
468
Vector Time (MET): N/A
Weight (LBS) : 883811
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1407766
37 A = 6758574
03 meter
Y = -5134229
51 meter E =
0007122
Z = 4169132
48 I = 51
95278
XDOT = 5015
258867 Wp = 354
13220
YDOT = -4431
966668 meter/sec RA = 112
46497 deg
ZDOT = -3758
088476 TA = 134
33827
MA = 134
27988
Ha = 207
896 n
mi
Hp = 204
378
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4618656
06 X = -1370502
72
Y = -16844585
02 feet Y = -5149764
27 meter
Z = 13678256
18 Z = 4162383
31
XDOT = 16454
261376 XDOT = 5082
701370
YDOT = -14540
573058 feet/sec YDOT = -4375
505355 meter/sec
ZDOT = -12329
686601 ZDOT = -3733
561130
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12102707
16 X = -3688905
14
Y = 12622946
70 feet Y = 3847474
15 meter
Z = 13651095
79 Z = 4160854
00
XDOT = -20010
621974 XDOT = -6099
237578
YDOT = -5937
295042 feet/sec YDOT = -1809
687529 meter/sec
ZDOT = -12229
919728 ZDOT = -3727
679533
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 11177
61634445
00016717 00000-0 10270-3 0 9041
2 25544 51
6406 113
1755 0011632 292
6724 67
3203 15
62195533 2386
Satellite: ISS
Catalog Number: 25544
Epoch time: 11177
61634445 = yrday
fracday
Element set: 904
Inclination: 51
6406 deg
RA of node: 113
1755 deg
Eccentricity:
0011632
Arg of perigee: 292
6724 deg
Mean anomaly: 67
3203 deg
Mean motion: 15
62195533 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 238
Checksum: 291
Coasting Arc #6 (Orbit 252)
---------------------------------------
Vector Time (GMT): 2011/178/13:48:14
468
Vector Time (MET): N/A
Weight (LBS) : 883811
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1755946
67 A = 6765857
35 meter
Y = 6514532
58 meter E =
0013924
Z = -357961
34 I = 51
98876
XDOT = -4660
357503 Wp = 348
31177
YDOT = -922
658218 meter/sec RA = 107
46177 deg
ZDOT = 6042
025711 TA = 7
83258
MA = 7
81085
Ha = 208
181 n
mi
Hp = 204
113
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5760979
90 X = -1826924
02
Y = 21373138
39 feet Y = 6494499
72 meter
Z = -1174413
84 Z = -366663
08
XDOT = -15289
886822 XDOT = -4679
044883
YDOT = -3027
093890 feet/sec YDOT = -974
878643 meter/sec
ZDOT = 19822
918998 ZDOT = 6019
340125
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21219186
51 X = 6467608
05
Y = -6297704
46 feet Y = -1919540
32 meter
Z = -1210051
44 Z = -368823
68
XDOT = 5036
711037 XDOT = 1535
189524
YDOT = 13162
513636 feet/sec YDOT = 4011
934156 meter/sec
ZDOT = 19730
869091 ZDOT = 6013
968899
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 11178
57587902
00016717 00000-0 10270-3 0 9053
2 25544 51
6414 108
3329 0011747 296
3406 63
6544 15
62219301 2537
Satellite: ISS
Catalog Number: 25544
Epoch time: 11178
57587902 = yrday
fracday
Element set: 905
Inclination: 51
6414 deg
RA of node: 108
3329 deg
Eccentricity:
0011747
Arg of perigee: 296
3406 deg
Mean anomaly: 63
6544 deg
Mean motion: 15
62219301 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 253
Checksum: 304
Coasting Arc #7 (Orbit 268)
---------------------------------------
Vector Time (GMT): 2011/179/13:48:14
468
Vector Time (MET): N/A
Weight (LBS) : 883811
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3869500
15 A = 6760053
51 meter
Y = -4138694
05 meter E =
0008341
Z = -3689445
47 I = 51
97857
XDOT = 2178
625563 Wp = 325
62349
YDOT = 5932
831530 meter/sec RA = 102
46790 deg
ZDOT = -4358
810130 TA = 258
21907
MA = 258
31265
Ha = 208
358 n
mi
Hp = 203
991
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12695210
46 X = 3933414
86
Y = -13578392
56 feet Y = -4095064
92 meter
Z = -12104479
89 Z = -3670492
96
XDOT = 7147
721663 XDOT = 2133
295853
YDOT = 19464
670374 feet/sec YDOT = 5956
941576 meter/sec
ZDOT = -14300
558170 ZDOT = -4348
335420
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18317516
82 X = -5583179
13
Y = -3445505
45 feet Y = -1050190
06 meter
Z = -12027327
89 Z = -3665929
54
XDOT = 12253
806485 XDOT = 3734
960217
YDOT = -15241
145888 feet/sec YDOT = -4645
501267 meter/sec
ZDOT = -14258
326609 ZDOT = -4345
937950
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 11179
59936533
00016717 00000-0 10270-3 0 9065
2 25544 51
6422 103
1684 0011817 299
9028 60
0955 15
62256371 2692
Satellite: ISS
Catalog Number: 25544
Epoch time: 11179
59936533 = yrday
fracday
Element set: 906
Inclination: 51
6422 deg
RA of node: 103
1684 deg
Eccentricity:
0011817
Arg of perigee: 299
9028 deg
Mean anomaly: 60
0955 deg
Mean motion: 15
62256371 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 269
Checksum: 321
Coasting Arc #8 (Orbit 283)
---------------------------------------
Vector Time (GMT): 2011/180/12:52:30
893
Vector Time (MET): N/A
Weight (LBS) : 882426
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3867601
62 A = 6765201
78 meter
Y = -3502258
90 meter E =
0000915
Z = -4306365
69 I = 51
97327
XDOT = 1935
864043 Wp = 330
69861
YDOT = 6518
207262 meter/sec RA = 97
63873 deg
ZDOT = -3561
373862 TA = 263
20967
MA = 263
22008
Ha = 210
989 n
mi
Hp = 209
336
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12688981
68 X = 3927396
54
Y = -11490350
71 feet Y = -3458673
88 meter
Z = -14128496
36 Z = -4287432
39
XDOT = 6351
259982 XDOT = 1880
132733
YDOT = 21385
194429 feet/sec YDOT = 6539
544335 meter/sec
ZDOT = -11684
297446 ZDOT = -3552
103613
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15110069
25 X = -4605549
11
Y = -8178974
42 feet Y = -2492951
40 meter
Z = -14051441
54 Z = -4282879
38
XDOT = 17395
218234 XDOT = 5302
062518
YDOT = -12120
726880 feet/sec YDOT = -3694
397553 meter/sec
ZDOT = -11646
992094 ZDOT = -3550
003190
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 11180
55892598
00016717 00000-0 10270-3 0 9076
2 25544 51
6386 98
3273 0008629 255
7276 104
2921 15
59750218 2848
Satellite: ISS
Catalog Number: 25544
Epoch time: 11180
55892598 = yrday
fracday
Element set: 907
Inclination: 51
6386 deg
RA of node: 98
3273 deg
Eccentricity:
0008629
Arg of perigee: 255
7276 deg
Mean anomaly: 104
2921 deg
Mean motion: 15
59750218 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 284
Checksum: 338
Coasting Arc #9 (Orbit 299)
---------------------------------------
Vector Time (GMT): 2011/181/12:52:30
893
Vector Time (MET): N/A
Weight (LBS) : 882426
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4145338
30 A = 6760942
86 meter
Y = -504228
79 meter E =
0006279
Z = 5322438
69 I = 51
96230
XDOT = 569
399300 Wp = 260
28941
YDOT = -7647
233871 meter/sec RA = 92
60781 deg
ZDOT = -282
313310 TA = 192
38022
MA = 192
39565
Ha = 210
706 n
mi
Hp = 209
501
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13600191
28 X = -4165247
02
Y = -1654293
94 feet Y = -550696
82 meter
Z = 17462069
19 Z = 5302252
37
XDOT = 1868
107940 XDOT = 656
241241
YDOT = -25089
349970 feet/sec YDOT = -7640
380888 meter/sec
ZDOT = -926
224771 ZDOT = -279
337723
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3270711
23 X = 996912
78
Y = 13411168
54 feet Y = 4087724
17 meter
Z = 17380125
38 Z = 5297462
22
XDOT = -23168
289574 XDOT = -7061
694662
YDOT = 6828
816443 feet/sec YDOT = 2081
423252 meter/sec
ZDOT = -913
738521 ZDOT = -278
507501
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 11181
58404896
00016717 00000-0 10270-3 0 9081
2 25544 51
6386 93
1731 0008790 259
5475 100
4690 15
59789806 3007
Satellite: ISS
Catalog Number: 25544
Epoch time: 11181
58404896 = yrday
fracday
Element set: 908
Inclination: 51
6386 deg
RA of node: 93
1731 deg
Eccentricity:
0008790
Arg of perigee: 259
5475 deg
Mean anomaly: 100
4690 deg
Mean motion: 15
59789806 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 300
Checksum: 332
Coasting Arc #10 (Orbit 314)
---------------------------------------
Vector Time (GMT): 2011/182/12:52:30
893
Vector Time (MET): N/A
Weight (LBS) : 882426
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3304347
12 A = 6766219
54 meter
Y = 4355019
94 meter E =
0003719
Z = -3987511
49 I = 51
98079
XDOT = -2890
717245 Wp = 215
77766
YDOT = 5870
336616 meter/sec RA = 87
58034 deg
ZDOT = 4011
094629 TA = 95
80199
MA = 95
75959
Ha = 210
408 n
mi
Hp = 209
765
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10841033
86 X = 3274773
20
Y = 14288123
17 feet Y = 4391806
54 meter
Z = -13082386
79 Z = -3971530
23
XDOT = -9483
980462 XDOT = -2975
630534
YDOT = 19259
634568 feet/sec YDOT = 5837
535346 meter/sec
ZDOT = 13159
759283 ZDOT = 3996
846546
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9272358
27 X = 2826214
80
Y = -15407454
50 feet Y = -4696192
13 meter
Z = -13017720
27 Z = -3967801
14
XDOT = 20303
633691 XDOT = 6188
547549
YDOT = 1136
010518 feet/sec YDOT = 346
256006 meter/sec
ZDOT = 13101
581169 ZDOT = 3993
361940
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 11182
54508975
00016717 00000-0 10270-3 0 9092
2 25544 51
6391 88
3408 0008763 263
5796 96
4362 15
59782959 3159
Satellite: ISS
Catalog Number: 25544
Epoch time: 11182
54508975 = yrday
fracday
Element set: 909
Inclination: 51
6391 deg
RA of node: 88
3408 deg
Eccentricity:
0008763
Arg of perigee: 263
5796 deg
Mean anomaly: 96
4362 deg
Mean motion: 15
59782959 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 315
Checksum: 355
Coasting Arc #11 (Orbit 330)
---------------------------------------
Vector Time (GMT): 2011/183/12:52:30
893
Vector Time (MET): N/A
Weight (LBS) : 882426
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1541314
74 A = 6772663
23 meter
Y = -6530033
03 meter E =
0008715
Z = 878863
13 I = 51
99983
XDOT = 4460
425173 Wp = 165
31798
YDOT = -1856
630278 meter/sec RA = 82
59321 deg
ZDOT = -5967
756787 TA = 5
19529
MA = 5
18626
Ha = 210
321 n
mi
Hp = 209
848
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5056806
90 X = -1472449
38
Y = -21423992
87 feet Y = -6546884
05 meter
Z = 2883409
23 Z = 871541
74
XDOT = 14633
940855 XDOT = 4509
844631
YDOT = -6091
306687 feet/sec YDOT = -1806
473775 meter/sec
ZDOT = -19579
254552 ZDOT = -5945
968692
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17838660
14 X = -5437223
61
Y = 12903857
17 feet Y = 3933095
67 meter
Z = 2854030
50 Z = 869908
50
XDOT = -10343
723086 XDOT = -3152
766797
YDOT = -9985
163013 feet/sec YDOT = -3043
477686 meter/sec
ZDOT = -19490
663698 ZDOT = -5940
754295
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 11183
57018537
00016717 00000-0 10270-3 0 9108
2 25544 51
6391 83
1868 0008757 266
3484 93
6671 15
59768022 3315
Satellite: ISS
Catalog Number: 25544
Epoch time: 11183
57018537 = yrday
fracday
Element set: 910
Inclination: 51
6391 deg
RA of node: 83
1868 deg
Eccentricity:
0008757
Arg of perigee: 266
3484 deg
Mean anomaly: 93
6671 deg
Mean motion: 15
59768022 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 331
Checksum: 327
Coasting Arc #12 (Orbit 346)
---------------------------------------
Vector Time (GMT): 2011/184/12:52:30
893
Vector Time (MET): N/A
Weight (LBS) : 882426
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -744464
22 A = 6769924
31 meter
Y = 6190506
45 meter E =
0005560
Z = 2628449
21 I = 51
98602
XDOT = -4829
149283 Wp = 53
59666
YDOT = -2816
661930 meter/sec RA = 77
61767 deg
ZDOT = 5261
531154 TA = 335
94429
MA = 335
97026
Ha = 210
042 n
mi
Hp = 209
762
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2442467
92 X = -826400
61
Y = 20310060
53 feet Y = 6181722
89 meter
Z = 8623521
02 Z = 2624634
55
XDOT = -15843
665625 XDOT = -4822
852977
YDOT = -9241
016830 feet/sec YDOT = -2870
629973 meter/sec
ZDOT = 17262
241320 ZDOT = 5238
086485
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19616268
04 X = 5979038
50
Y = -5825726
24 feet Y = -1775681
36 meter
Z = 8607686
40 Z = 2623622
81
XDOT = -2526
354288 XDOT = -770
032787
YDOT = 16880
070129 feet/sec YDOT = 5145
045375 meter/sec
ZDOT = 17167
173427 ZDOT = 5232
554461
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 11184
59526429
00016717 00000-0 10270-3 0 9116
2 25544 51
6389 78
0315 0008824 272
0979 87
9167 15
59810416 3478
Satellite: ISS
Catalog Number: 25544
Epoch time: 11184
59526429 = yrday
fracday
Element set: 911
Inclination: 51
6389 deg
RA of node: 78
0315 deg
Eccentricity:
0008824
Arg of perigee: 272
0979 deg
Mean anomaly: 87
9167 deg
Mean motion: 15
59810416 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 347
Checksum: 338
Coasting Arc #13 (Orbit 361)
---------------------------------------
Vector Time (GMT): 2011/185/12:52:30
893
Vector Time (MET): N/A
Weight (LBS) : 882426
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2969362
54 A = 6762273
69 meter
Y = -3511490
89 meter E =
0005267
Z = -4961932
02 I = 51
95295
XDOT = 3778
919801 Wp = 35
00959
YDOT = 6306
963028 meter/sec RA = 72
60727 deg
ZDOT = -2198
882643 TA = 213
63716
MA = 213
67061
Ha = 210
091 n
mi
Hp = 209
435
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9742003
10 X = 3032511
73
Y = -11520639
39 feet Y = -3477931
98 meter
Z = -16279304
52 Z = -4947354
17
XDOT = 12398
030843 XDOT = 3718
794831
YDOT = 20692
135920 feet/sec YDOT = 6348
885299 meter/sec
ZDOT = -7214
181898 ZDOT = -2180
670274
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14566497
87 X = -4439868
55
Y = -4168880
57 feet Y = -1270674
80 meter
Z = -16219897
87 Z = -4943824
87
XDOT = 13355
933955 XDOT = 4070
888669
YDOT = -18846
051804 feet/sec YDOT = -5744
276590 meter/sec
ZDOT = -7140
558347 ZDOT = -2176
442184
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 11185
55626134
00016717 00000-0 10270-3 0 9128
2 25544 51
6385 73
1989 0008990 275
6939 84
3191 15
59863428 3622
Satellite: ISS
Catalog Number: 25544
Epoch time: 11185
55626134 = yrday
fracday
Element set: 912
Inclination: 51
6385 deg
RA of node: 73
1989 deg
Eccentricity:
0008990
Arg of perigee: 275
6939 deg
Mean anomaly: 84
3191 deg
Mean motion: 15
59863428 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 362
Checksum: 344
Coasting Arc #14 (Orbit 377)
---------------------------------------
Vector Time (GMT): 2011/186/12:52:30
893
Vector Time (MET): N/A
Weight (LBS) : 882426
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4461614
88 A = 6761746
62 meter
Y = -405799
03 meter E =
0006338
Z = 5069663
39 I = 51
94161
XDOT = -1445
416921 Wp = 316
36299
YDOT = -7304
686291 meter/sec RA = 67
56833 deg
ZDOT = -1853
659362 TA = 151
52044
MA = 151
48579
Ha = 210
447 n
mi
Hp = 209
434
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14637844
09 X = -4481372
65
Y = -1331361
66 feet Y = -455802
51 meter
Z = 16632753
90 Z = 5047941
19
XDOT = -4742
181498 XDOT = -1354
622490
YDOT = -23965
506203 feet/sec YDOT = -7320
341974 meter/sec
ZDOT = -6081
559586 ZDOT = -1860
461286
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5146893
21 X = 1568773
05
Y = 13873536
30 feet Y = 4228653
86 meter
Z = 16544545
52 Z = 5042777
48
XDOT = -18590
407397 XDOT = -5666
356175
YDOT = 14193
841041 feet/sec YDOT = 4326
282749 meter/sec
ZDOT = -6108
777151 ZDOT = -1861
955276
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 11186
58131110
00016717 00000-0 10270-3 0 9138
2 25544 51
6387 68
0439 0009072 279
3241 80
6889 15
59900822 3786
Satellite: ISS
Catalog Number: 25544
Epoch time: 11186
58131110 = yrday
fracday
Element set: 913
Inclination: 51
6387 deg
RA of node: 68
0439 deg
Eccentricity:
0009072
Arg of perigee: 279
3241 deg
Mean anomaly: 80
6889 deg
Mean motion: 15
59900822 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 378
Checksum: 318
Coasting Arc #15 (Orbit 392)
---------------------------------------
Vector Time (GMT): 2011/187/12:52:30
893
Vector Time (MET): N/A
Weight (LBS) : 882426
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4626924
19 A = 6769142
00 meter
Y = 4000225
50 meter E =
0006362
Z = -2890520
30 I = 51
95288
XDOT = -1606
370001 Wp = 310
84806
YDOT = 5530
187281 meter/sec RA = 62
55161 deg
ZDOT = 5078
732285 TA = 16
29326
MA = 16
27282
Ha = 210
741 n
mi
Hp = 209
108
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15180197
47 X = 4595890
45
Y = 13124099
43 feet Y = 4051793
33 meter
Z = -9483334
30 Z = -2868118
01
XDOT = -5270
242787 XDOT = -1692
761479
YDOT = 18143
659060 feet/sec YDOT = 5511
740376 meter/sec
ZDOT = 16662
507498 ZDOT = 5070
719296
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4946579
69 X = 1507717
49
Y = -19491664
88 feet Y = -5941059
46 meter
Z = -9392569
40 Z = -2862855
15
XDOT = 17213
047332 XDOT = 5246
536827
YDOT = -3650
232687 feet/sec YDOT = -1112
590923 meter/sec
ZDOT = 16629
644750 ZDOT = 5068
715720
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 11187
54228307
00016717 00000-0 10270-3 0 9141
2 25544 51
6379 63
2101 0009169 283
1497 76
8635 15
59885831 3938
Satellite: ISS
Catalog Number: 25544
Epoch time: 11187
54228307 = yrday
fracday
Element set: 914
Inclination: 51
6379 deg
RA of node: 63
2101 deg
Eccentricity:
0009169
Arg of perigee: 283
1497 deg
Mean anomaly: 76
8635 deg
Mean motion: 15
59885831 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 393
Checksum: 333
Coasting Arc #16 (Orbit 408)
---------------------------------------
Vector Time (GMT): 2011/188/12:52:30
893
Vector Time (MET): N/A
Weight (LBS) : 882426
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3208035
17 A = 6772489
88 meter
Y = -5929441
44 meter E =
0005946
Z = -602685
28 I = 51
94922
XDOT = 4433
800777 Wp = 196
93243
YDOT = -1787
437965 meter/sec RA = 57
57265 deg
ZDOT = -6005
930049 TA = 349
56015
MA = 349
57250
Ha = 210
809 n
mi
Hp = 209
009
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10525049
76 X = -3138564
86
Y = -19453548
03 feet Y = -5964927
16 meter
Z = -1977313
90 Z = -618101
58
XDOT = 14546
590476 XDOT = 4482
634196
YDOT = -5864
297786 feet/sec YDOT = -1737
582917 meter/sec
ZDOT = -19704
494911 ZDOT = -5984
272373
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12406276
44 X = -3781433
06
Y = 18304408
51 feet Y = 5579183
71 meter
Z = -2039585
10 Z = -621665
54
XDOT = -10636
368204 XDOT = -3241
965029
YDOT = -9398
135223 feet/sec YDOT = -2864
551616 meter/sec
ZDOT = -19616
422901 ZDOT = -5979
085700
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 11188
56730571
00016717 00000-0 10270-3 0 9156
2 25544 51
6378 58
0555 0009110 286
0292 73
9860 15
59881966 4094
Satellite: ISS
Catalog Number: 25544
Epoch time: 11188
56730571 = yrday
fracday
Element set: 915
Inclination: 51
6378 deg
RA of node: 58
0555 deg
Eccentricity:
0009110
Arg of perigee: 286
0292 deg
Mean anomaly: 73
9860 deg
Mean motion: 15
59881966 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 409
Checksum: 334
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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