[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
September 17th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15069 47 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 1510)
---------------------------------------
Vector Time (GMT): 2011/259/03:24:10
567
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3631708
29 A = 6768819
00 meter
Y = 5666883
88 meter E =
0004172
Z = -735545
93 I = 51
96404
XDOT = -3651
785860 Wp = 127
00683
YDOT = 3114
407136 meter/sec RA = 62
24984 deg
ZDOT = 5984
815338 TA = 225
06525
MA = 225
09909
Ha = 212
047 n
mi
Hp = 203
472
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11915053
45 X = 3571643
33
Y = 18592138
72 feet Y = 5707159
96 meter
Z = -2413208
44 Z = -718049
40
XDOT = -11980
924737 XDOT = -3715
413667
YDOT = 10217
871180 feet/sec YDOT = 3073
215392 meter/sec
ZDOT = 19635
220924 ZDOT = 5966
920046
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21580993
99 X = 6577886
97
Y = 4715332
90 feet Y = 1437233
47 meter
Z = -2342227
58 Z = -713910
97
XDOT = -988
719702 XDOT = -301
361765
YDOT = 14207
146707 feet/sec YDOT = 4330
338316 meter/sec
ZDOT = 19562
161092 ZDOT = 5962
546701
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 11259
14316919
00016717 00000-0 10270-3 0 9009
2 25544 51
6378 62
9154 0011151 198
0648 162
0114 15
61132288 15114
Satellite: ISS
Catalog Number: 25544
Epoch time: 11259
14316919 = yrday
fracday
Element set: 900
Inclination: 51
6378 deg
RA of node: 62
9154 deg
Eccentricity:
0011151
Arg of perigee: 198
0648 deg
Mean anomaly: 162
0114 deg
Mean motion: 15
61132288 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1511
Checksum: 287
Coasting Arc #2 (Orbit 1526)
---------------------------------------
Vector Time (GMT): 2011/260/03:24:10
567
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -890115
05 A = 6764706
51 meter
Y = -5921892
31 meter E =
0011263
Z = -3133475
07 I = 51
93694
XDOT = 5666
241248 Wp = 178
29404
YDOT = 1730
564056 meter/sec RA = 57
26335 deg
ZDOT = -4891
571876 TA = 37
78153
MA = 37
70252
Ha = 211
810 n
mi
Hp = 203
609
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2920324
98 X = -808607
18
Y = -19428780
53 feet Y = -5931390
61 meter
Z = -10280430
01 Z = -3137600
86
XDOT = 18590
030341 XDOT = 5670
231136
YDOT = 5677
703597 feet/sec YDOT = 1793
949385 meter/sec
ZDOT = -16048
464160 ZDOT = -4864
035539
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15956727
67 X = -4863610
59
Y = -11447678
24 feet Y = -3489252
33 meter
Z = -10296919
79 Z = -3138501
15
XDOT = 16233
760839 XDOT = 4948
050304
YDOT = -8327
220829 feet/sec YDOT = -2538
136909 meter/sec
ZDOT = -15936
385339 ZDOT = -4857
410251
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 11260
16736829
00016717 00000-0 10270-3 0 9010
2 25544 51
6391 57
7550 0011047 202
0595 158
0087 15
61173356 15274
Satellite: ISS
Catalog Number: 25544
Epoch time: 11260
16736829 = yrday
fracday
Element set: 901
Inclination: 51
6391 deg
RA of node: 57
7550 deg
Eccentricity:
0011047
Arg of perigee: 202
0595 deg
Mean anomaly: 158
0087 deg
Mean motion: 15
61173356 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1527
Checksum: 298
Coasting Arc #3 (Orbit 1542)
---------------------------------------
Vector Time (GMT): 2011/261/03:24:10
567
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2514142
75 A = 6757111
80 meter
Y = 3458813
77 meter E =
0012084
Z = 5235416
48 I = 51
89464
XDOT = -5286
868628 Wp = 188
56135
YDOT = -5465
223170 meter/sec RA = 52
22940 deg
ZDOT = 1060
438020 TA = 251
26340
MA = 251
39457
Ha = 211
580 n
mi
Hp = 203
828
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8248499
82 X = -2578065
88
Y = 11347814
20 feet Y = 3430341
98 meter
Z = 17176563
26 Z = 5223047
23
XDOT = -17345
369514 XDOT = -5230
513944
YDOT = -17930
522210 feet/sec YDOT = -5524
029011 meter/sec
ZDOT = 3479
127363 ZDOT = 1034
891466
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2594282
52 X = 790737
31
Y = 13849739
48 feet Y = 4221400
59 meter
Z = 17125985
42 Z = 5220000
36
XDOT = -23947
420048 XDOT = -7299
173631
YDOT = 265
740963 feet/sec YDOT = 80
997846 meter/sec
ZDOT = 3375
363389 ZDOT = 1028
810761
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 11261
19154616
00016717 00000-0 10270-3 0 9023
2 25544 51
6391 52
5951 0011115 206
6265 153
4322 15
61228361 15438
Satellite: ISS
Catalog Number: 25544
Epoch time: 11261
19154616 = yrday
fracday
Element set: 902
Inclination: 51
6391 deg
RA of node: 52
5951 deg
Eccentricity:
0011115
Arg of perigee: 206
6265 deg
Mean anomaly: 153
4322 deg
Mean motion: 15
61228361 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1543
Checksum: 275
Coasting Arc #4 (Orbit 1557)
---------------------------------------
Vector Time (GMT): 2011/262/03:24:10
567
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5115991
97 A = 6760577
33 meter
Y = 432900
28 meter E =
0012946
Z = -4408153
15 I = 51
88727
XDOT = 2374
801761 Wp = 166
64095
YDOT = 6463
685213 meter/sec RA = 47
17569 deg
ZDOT = 3380
582685 TA = 137
47192
MA = 137
37157
Ha = 211
351 n
mi
Hp = 204
167
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16784750
57 X = 5132185
07
Y = 1420276
50 feet Y = 490200
76 meter
Z = -14462444
73 Z = -4383260
24
XDOT = 7791
344359 XDOT = 2285
924731
YDOT = 21206
316317 feet/sec YDOT = 6489
744920 meter/sec
ZDOT = 11091
150542 ZDOT = 3391
903334
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12355225
84 X = 3765872
84
Y = -11576507
43 feet Y = -3528519
47 meter
Z = -14361065
93 Z = -4377252
90
XDOT = 20076
189946 XDOT = 6119
222696
YDOT = 7568
660532 feet/sec YDOT = 2306
927730 meter/sec
ZDOT = 11136
899855 ZDOT = 3394
527076
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 11262
15169672
00016717 00000-0 10270-3 0 9039
2 25544 51
6397 47
7565 0010924 210
0344 150
0190 15
61232581 15586
Satellite: ISS
Catalog Number: 25544
Epoch time: 11262
15169672 = yrday
fracday
Element set: 903
Inclination: 51
6397 deg
RA of node: 47
7565 deg
Eccentricity:
0010924
Arg of perigee: 210
0344 deg
Mean anomaly: 150
0190 deg
Mean motion: 15
61232581 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1558
Checksum: 289
Coasting Arc #5 (Orbit 1573)
---------------------------------------
Vector Time (GMT): 2011/263/03:24:10
567
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5473069
74 A = 6768274
20 meter
Y = -3810887
33 meter E =
0017475
Z = 1083121
62 I = 51
89203
XDOT = 1956
045024 Wp = 162
03915
YDOT = -4494
855649 meter/sec RA = 42
16768 deg
ZDOT = -5921
794358 TA = 6
20547
MA = 6
18385
Ha = 211
196 n
mi
Hp = 204
252
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17956265
55 X = -5435310
49
Y = -12502911
20 feet Y = -3871879
38 meter
Z = 3553548
62 Z = 1056625
28
XDOT = 6417
470550 XDOT = 2034
929061
YDOT = -14746
901736 feet/sec YDOT = -4472
541136 meter/sec
ZDOT = -19428
459179 ZDOT = -5912
100080
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21236553
76 X = -6472901
58
Y = 5339755
35 feet Y = 1627557
43 meter
Z = 3445833
13 Z = 1050289
94
XDOT = -6436
471388 XDOT = -1961
836479
YDOT = -13066
664957 feet/sec YDOT = -3982
719479 meter/sec
ZDOT = -19388
708308 ZDOT = -5909
678292
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 11263
17583641
00016717 00000-0 10270-3 0 9049
2 25544 51
6400 42
5961 0010935 213
9004 146
1455 15
61238774 15749
Satellite: ISS
Catalog Number: 25544
Epoch time: 11263
17583641 = yrday
fracday
Element set: 904
Inclination: 51
6400 deg
RA of node: 42
5961 deg
Eccentricity:
0010935
Arg of perigee: 213
9004 deg
Mean anomaly: 146
1455 deg
Mean motion: 15
61238774 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1574
Checksum: 292
Coasting Arc #6 (Orbit 1589)
---------------------------------------
Vector Time (GMT): 2011/264/03:24:10
567
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3193268
40 A = 6765082
38 meter
Y = 5237038
70 meter E =
0009160
Z = 2856508
74 I = 51
85879
XDOT = -5702
108891 Wp = 134
10124
YDOT = 691
748048 meter/sec RA = 37
17694 deg
ZDOT = 5089
799448 TA = 258
36284
MA = 258
46566
Ha = 210
825 n
mi
Hp = 204
467
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10476602
37 X = 3120593
09
Y = 17181885
49 feet Y = 5272341
55 meter
Z = 9371747
82 Z = 2871844
86
XDOT = -18707
706335 XDOT = -5734
145650
YDOT = 2269
514592 feet/sec YDOT = 627
804665 meter/sec
ZDOT = 16698
817085 ZDOT = 5062
020797
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19855772
11 X = 6052039
34
Y = 3091215
69 feet Y = 942202
54 meter
Z = 9433914
50 Z = 2875457
14
XDOT = -10147
951358 XDOT = -3093
095574
YDOT = 14404
225959 feet/sec YDOT = 4390
408072 meter/sec
ZDOT = 16585
615902 ZDOT = 5055
295727
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 11264
19995434
00016717 00000-0 10270-3 0 9050
2 25544 51
6400 37
4349 0010774 218
4450 141
5940 15
61282097 15901
Satellite: ISS
Catalog Number: 25544
Epoch time: 11264
19995434 = yrday
fracday
Element set: 905
Inclination: 51
6400 deg
RA of node: 37
4349 deg
Eccentricity:
0010774
Arg of perigee: 218
4450 deg
Mean anomaly: 141
5940 deg
Mean motion: 15
61282097 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1590
Checksum: 305
Coasting Arc #7 (Orbit 1604)
---------------------------------------
Vector Time (GMT): 2011/265/03:24:10
567
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 885905
07 A = 6756986
29 meter
Y = -4254680
24 meter E =
0008567
Z = -5178577
17 I = 51
80793
XDOT = 6901
107196 Wp = 129
25534
YDOT = 3077
217083 meter/sec RA = 32
13878 deg
ZDOT = -1354
424834 TA = 127
81049
MA = 127
73290
Ha = 210
553 n
mi
Hp = 204
654
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2906512
70 X = 958572
38
Y = -13958924
66 feet Y = -4244367
47 meter
Z = -16990082
59 Z = -5174096
74
XDOT = 22641
427809 XDOT = 6872
763767
YDOT = 10095
856573 feet/sec YDOT = 3154
230940 meter/sec
ZDOT = -4443
651030 ZDOT = -1320
968404
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8936292
14 X = -2723781
84
Y = -11138693
17 feet Y = -3395073
68 meter
Z = -16971579
11 Z = -5172937
31
XDOT = 21317
954996 XDOT = 6497
712683
YDOT = -10573
588973 feet/sec YDOT = -3222
829919 meter/sec
ZDOT = -4307
542868 ZDOT = -1312
939066
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 11265
16004495
00016717 00000-0 10270-3 0 9067
2 25544 51
6406 32
5964 0010721 222
5499 137
4827 15
61343975 16055
Satellite: ISS
Catalog Number: 25544
Epoch time: 11265
16004495 = yrday
fracday
Element set: 906
Inclination: 51
6406 deg
RA of node: 32
5964 deg
Eccentricity:
0010721
Arg of perigee: 222
5499 deg
Mean anomaly: 137
4827 deg
Mean motion: 15
61343975 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1605
Checksum: 306
Coasting Arc #8 (Orbit 1620)
---------------------------------------
Vector Time (GMT): 2011/266/03:24:10
567
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4764399
77 A = 6759656
64 meter
Y = 1568346
63 meter E =
0003902
Z = 4528992
09 I = 51
79062
XDOT = -4702
206128 Wp = 173
44712
YDOT = -5191
022660 meter/sec RA = 27
07735 deg
ZDOT = -3152
537691 TA = 308
02530
MA = 308
06051
Ha = 210
317 n
mi
Hp = 204
901
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15631232
84 X = -4803584
12
Y = 5145494
19 feet Y = 1514849
41 meter
Z = 14858897
93 Z = 4505751
49
XDOT = -15427
185460 XDOT = -4628
495249
YDOT = -17030
914238 feet/sec YDOT = -5243
193683 meter/sec
ZDOT = -10342
971426 ZDOT = -3175
201467
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5653582
31 X = -1723211
89
Y = 15545283
19 feet Y = 4738202
32 meter
Z = 14764131
39 Z = 4500107
25
XDOT = -21749
831405 XDOT = -6629
348612
YDOT = 1989
501451 feet/sec YDOT = 606
400042 meter/sec
ZDOT = -10434
987357 ZDOT = -3180
584147
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 11266
18412130
00016717 00000-0 10270-3 0 9070
2 25544 51
6405 27
4354 0010680 227
2564 132
7694 15
61379987 16219
Satellite: ISS
Catalog Number: 25544
Epoch time: 11266
18412130 = yrday
fracday
Element set: 907
Inclination: 51
6405 deg
RA of node: 27
4354 deg
Eccentricity:
0010680
Arg of perigee: 227
2564 deg
Mean anomaly: 132
7694 deg
Mean motion: 15
61379987 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1621
Checksum: 303
Coasting Arc #9 (Orbit 1635)
---------------------------------------
Vector Time (GMT): 2011/267/03:24:10
567
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6465468
56 A = 6767614
04 meter
Y = 1544032
14 meter E =
0002768
Z = -1266586
11 I = 51
79065
XDOT = -35
178743 Wp = 279
53076
YDOT = 4960
407022 meter/sec RA = 22
05783 deg
ZDOT = 5856
986509 TA = 66
68835
MA = 66
65922
Ha = 209
985 n
mi
Hp = 205
122
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21212167
19 X = 6453875
17
Y = 5065722
23 feet Y = 1616268
02 meter
Z = -4155466
23 Z = -1235205
36
XDOT = -115
415823 XDOT = -119
096380
YDOT = 16274
301252 feet/sec YDOT = 4959
544960 meter/sec
ZDOT = 19215
835002 ZDOT = 5856
611321
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16856731
01 X = 5137931
61
Y = -13874923
79 feet Y = -4229076
77 meter
Z = -4027727
35 Z = -1227651
29
XDOT = 11825
013983 XDOT = 3604
264262
YDOT = 8778
438005 feet/sec YDOT = 2675
667904 meter/sec
ZDOT = 19214
012892 ZDOT = 5856
431129
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 11267
14417366
00016717 00000-0 10270-3 0 9084
2 25544 51
6411 22
5959 0010701 230
9639 129
0565 15
61403647 16364
Satellite: ISS
Catalog Number: 25544
Epoch time: 11267
14417366 = yrday
fracday
Element set: 908
Inclination: 51
6411 deg
RA of node: 22
5959 deg
Eccentricity:
0010701
Arg of perigee: 230
9639 deg
Mean anomaly: 129
0565 deg
Mean motion: 15
61403647 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1636
Checksum: 302
Coasting Arc #10 (Orbit 1651)
---------------------------------------
Vector Time (GMT): 2011/268/03:24:10
567
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4904791
20 A = 6765022
68 meter
Y = -3760152
08 meter E =
0009887
Z = -2734853
83 I = 51
75363
XDOT = 4980
579810 Wp = 208
78174
YDOT = -2735
717763 meter/sec RA = 17
06060 deg
ZDOT = -5171
752770 TA = 2
23318
MA = 2
22877
Ha = 209
735 n
mi
Hp = 205
281
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16091834
65 X = -4849094
53
Y = -12336456
96 feet Y = -3814689
36 meter
Z = -8972617
55 Z = -2758545
48
XDOT = 16340
484942 XDOT = 5035
924313
YDOT = -8975
451979 feet/sec YDOT = -2679
713017 meter/sec
ZDOT = -16967
692816 ZDOT = -5147
422472
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19421293
72 X = -5919610
33
Y = 5675525
01 feet Y = 1729900
02 meter
Z = -9068899
84 Z = -2764200
67
XDOT = 2862
120356 XDOT = 872
374284
YDOT = -17156
204327 feet/sec YDOT = -5229
211079 meter/sec
ZDOT = -16868
425386 ZDOT = -5141
496058
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 11268
16820832
00016717 00000-0 10270-3 0 9094
2 25544 51
6412 17
4348 0010827 235
3848 124
6288 15
61392655 16527
Satellite: ISS
Catalog Number: 25544
Epoch time: 11268
16820832 = yrday
fracday
Element set: 909
Inclination: 51
6412 deg
RA of node: 17
4348 deg
Eccentricity:
0010827
Arg of perigee: 235
3848 deg
Mean anomaly: 124
6288 deg
Mean motion: 15
61392655 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1652
Checksum: 315
Coasting Arc #11 (Orbit 1667)
---------------------------------------
Vector Time (GMT): 2011/269/03:24:10
567
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 772204
26 A = 6756804
59 meter
Y = 4318938
00 meter E =
0009649
Z = 5144896
57 I = 51
69748
XDOT = -7521
737648 Wp = 213
46811
YDOT = -413
962977 meter/sec RA = 12
01550 deg
ZDOT = 1469
889233 TA = 222
36937
MA = 222
44393
Ha = 209
406 n
mi
Hp = 205
482
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2533478
56 X = 698858
67
Y = 14169744
10 feet Y = 4327163
84 meter
Z = 16879581
94 Z = 5148469
22
XDOT = -24677
616955 XDOT = -7523
690056
YDOT = -1358
146250 feet/sec YDOT = -498
086379 meter/sec
ZDOT = 4822
471236 ZDOT = 1433
343940
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12985938
52 X = 3958114
06
Y = 6171119
34 feet Y = 1880957
18 meter
Z = 16893878
61 Z = 5149254
20
XDOT = -14885
797289 XDOT = -4537
191014
YDOT = 18470
974958 feet/sec YDOT = 5629
953167 meter/sec
ZDOT = 4673
643022 ZDOT = 1424
526393
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 11269
19222121
00016717 00000-0 10270-3 0 9107
2 25544 51
6415 12
2730 0010570 239
5138 120
4976 15
61446156 16682
Satellite: ISS
Catalog Number: 25544
Epoch time: 11269
19222121 = yrday
fracday
Element set: 910
Inclination: 51
6415 deg
RA of node: 12
2730 deg
Eccentricity:
0010570
Arg of perigee: 239
5138 deg
Mean anomaly: 120
4976 deg
Mean motion: 15
61446156 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1668
Checksum: 283
Coasting Arc #12 (Orbit 1682)
---------------------------------------
Vector Time (GMT): 2011/270/03:24:10
567
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3891243
05 A = 6759241
63 meter
Y = -3147023
14 meter E =
0008109
Z = -4547261
61 I = 51
67557
XDOT = 6238
621595 Wp = 182
09684
YDOT = 3226
360550 meter/sec RA = 6
94356 deg
ZDOT = 3097
622487 TA = 118
89946
MA = 118
81809
Ha = 209
115 n
mi
Hp = 205
653
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12766545
45 X = 3948234
39
Y = -10324879
07 feet Y = -3103190
82 meter
Z = -14918837
30 Z = -4528218
99
XDOT = 20467
918620 XDOT = 6187
032343
YDOT = 10585
172407 feet/sec YDOT = 3295
836596 meter/sec
ZDOT = 10162
803434 ZDOT = 3127
804150
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1322618
80 X = -403134
21
Y = -16436305
64 feet Y = -5009785
96 meter
Z = -14841093
41 Z = -4523565
27
XDOT = 19020
792514 XDOT = 5797
537558
YDOT = -10842
012861 feet/sec YDOT = -3304
645520 meter/sec
ZDOT = 10285
536087 ZDOT = 3135
031399
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 11270
15221255
00016717 00000-0 10270-3 0 9113
2 25544 51
6411 7
4333 0010660 243
9955 116
0104 15
61497247 16837
Satellite: ISS
Catalog Number: 25544
Epoch time: 11270
15221255 = yrday
fracday
Element set: 911
Inclination: 51
6411 deg
RA of node: 7
4333 deg
Eccentricity:
0010660
Arg of perigee: 243
9955 deg
Mean anomaly: 116
0104 deg
Mean motion: 15
61497247 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1683
Checksum: 274
Coasting Arc #13 (Orbit 1698)
---------------------------------------
Vector Time (GMT): 2011/271/03:24:10
567
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6590879
54 A = 6767331
28 meter
Y = 789207
55 meter E =
0011430
Z = 1276624
15 I = 51
67266
XDOT = -1693
561709 Wp = 169
29460
YDOT = -4684
106383 meter/sec RA = 1
91669 deg
ZDOT = -5850
324049 TA = 356
77481
MA = 356
78218
Ha = 208
878 n
mi
Hp = 205
775
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21623620
53 X = -6605416
44
Y = 2589263
61 feet Y = 715423
17 meter
Z = 4188399
46 Z = 1244569
90
XDOT = -5556
304818 XDOT = -1612
637094
YDOT = -15367
803093 feet/sec YDOT = -4702
593045 meter/sec
ZDOT = -19193
976538 ZDOT = -5858
354342
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9681564
25 X = -2950940
78
Y = 19535338
05 feet Y = 5954371
04 meter
Z = 4057809
99 Z = 1236820
48
XDOT = -14415
559308 XDOT = -4393
862477
YDOT = -3152
440856 feet/sec YDOT = -960
863973 meter/sec
ZDOT = -19226
398784 ZDOT = -5860
206349
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
17618392
00016717 00000-0 10270-3 0 9129
2 25544 51
6412 2
2725 0010550 247
5677 112
4363 15
61500779 16994
Satellite: ISS
Catalog Number: 25544
Epoch time: 11271
17618392 = yrday
fracday
Element set: 912
Inclination: 51
6412 deg
RA of node: 2
2725 deg
Eccentricity:
0010550
Arg of perigee: 247
5677 deg
Mean anomaly: 112
4363 deg
Mean motion: 15
61500779 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1699
Checksum: 297
Coasting Arc #14 (Orbit 1714)
---------------------------------------
Vector Time (GMT): 2011/272/03:24:10
567
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5885865
09 A = 6764482
22 meter
Y = 1869503
84 meter E =
0003208
Z = 2758912
49 I = 51
63249
XDOT = -3770
672146 Wp = 105
20835
YDOT = 4278
293281 meter/sec RA = 356
90920 deg
ZDOT = 5139
482517 TA = 286
13977
MA = 286
17507
Ha = 208
394 n
mi
Hp = 205
725
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19310580
99 X = 5851119
97
Y = 6133542
79 feet Y = 1935129
18 meter
Z = 9051550
18 Z = 2787421
87
XDOT = -12370
971606 XDOT = -3843
199661
YDOT = 14036
395278 feet/sec YDOT = 4235
722273 meter/sec
ZDOT = 16861
819283 ZDOT = 5120
987753
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15450959
99 X = 4709452
60
Y = -13025881
15 feet Y = -3970288
57 meter
Z = 9167535
21 Z = 2794264
73
XDOT = 4282
688184 XDOT = 1305
363359
YDOT = 16907
287812 feet/sec YDOT = 5153
341325 meter/sec
ZDOT = 16786
241843 ZDOT = 5116
446514
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
20013112
00016717 00000-0 10270-3 0 9134
2 25544 51
6402 357
1094 0010666 252
6283 107
3708 15
61556939 17156
Satellite: ISS
Catalog Number: 25544
Epoch time: 11272
20013112 = yrday
fracday
Element set: 913
Inclination: 51
6402 deg
RA of node: 357
1094 deg
Eccentricity:
0010666
Arg of perigee: 252
6283 deg
Mean anomaly: 107
3708 deg
Mean motion: 15
61556939 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1715
Checksum: 284
Coasting Arc #15 (Orbit 1729)
---------------------------------------
Vector Time (GMT): 2011/273/03:24:10
567
Vector Time (MET): N/A
Weight (LBS) : 871443
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2109408
64 A = 6756293
32 meter
Y = -3828947
15 meter E =
0003523
Z = -5154448
90 I = 51
57366
XDOT = 7244
590078 Wp = 90
26924
YDOT = -2139
857041 meter/sec RA = 351
85339 deg
ZDOT = -1376
028356 TA = 166
51159
MA = 166
50217
Ha = 208
000 n
mi
Hp = 205
840
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6920632
04 X = -2041396
07
Y = -12562162
56 feet Y = -3852155
91 meter
Z = -16910921
60 Z = -5164531
11
XDOT = 23768
340150 XDOT = 7274
664537
YDOT = -7020
528350 feet/sec YDOT = -2058
675535 meter/sec
ZDOT = -4514
528727 ZDOT = -1340
760418
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14277960
62 X = -4351922
40
Y = -678726
54 feet Y = -206875
85 meter
Z = -16951740
80 Z = -5166890
60
XDOT = 6276
928776 XDOT = 1913
207891
YDOT = -22947
904114 feet/sec YDOT = -6994
521174 meter/sec
ZDOT = -4370
779062 ZDOT = -1332
213458
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
16006282
00016717 00000-0 10270-3 0 9141
2 25544 51
6389 352
2694 0010583 256
3033 103
6945 15
61590743 17304
Satellite: ISS
Catalog Number: 25544
Epoch time: 11273
16006282 = yrday
fracday
Element set: 914
Inclination: 51
6389 deg
RA of node: 352
2694 deg
Eccentricity:
0010583
Arg of perigee: 256
3033 deg
Mean anomaly: 103
6945 deg
Mean motion: 15
61590743 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1730
Checksum: 299
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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