[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
June 14th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 12916 69 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 102 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 235 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
166/15:05:17
457 8
6 9
5 9
5
N/A -3
6 0
3 203
5
000/00:30:34
915 1
7 0
6 197
7
166/19:08:44
067 -8
0 8
9 8
9
N/A -1
3 0
2 207
7
000/00:37:28
135 3
6 -0
4 205
3
Coasting Arc #1 (Orbit 22)
---------------------------------------
Vector Time (GMT): 2011/163/19:49:13
933
Vector Time (MET): N/A
Weight (LBS) : 919843
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -957052
28 A = 6737903
80 meter
Y = -4165760
78 meter E =
0011454
Z = 5215200
08 I = 51
60647
XDOT = 7606
250624 Wp = 211
89509
YDOT = -522
402822 meter/sec RA = 181
85712 deg
ZDOT = 969
988932 TA = 228
78892
MA = 228
88771
Ha = 200
303 n
mi
Hp = 194
592
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3139935
32 X = -935733
56
Y = -13667194
17 feet Y = -4176344
73 meter
Z = 17110236
49 Z = 5210601
81
XDOT = 24954
890498 XDOT = 7606
814838
YDOT = -1713
920021 feet/sec YDOT = -437
342104 meter/sec
ZDOT = 3182
378385 ZDOT = 1006
941755
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7161705
22 X = 2182887
75
Y = 12082789
17 feet Y = 3682834
14 meter
Z = 17091745
58 Z = 5209564
05
XDOT = -22415
223586 XDOT = -6832
160149
YDOT = 8532
589967 feet/sec YDOT = 2600
733422 meter/sec
ZDOT = 3332
176950 ZDOT = 1015
647534
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 11163
87537142
00016717 00000-0 10270-3 0 9006
2 25544 51
6403 182
6560 0011941 229
4231 130
5891 15
67896089 239
Satellite: ISS
Catalog Number: 25544
Epoch time: 11163
87537142 = yrday
fracday
Element set: 900
Inclination: 51
6403 deg
RA of node: 182
6560 deg
Eccentricity:
0011941
Arg of perigee: 229
4231 deg
Mean anomaly: 130
5891 deg
Mean motion: 15
67896089 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 23
Checksum: 299
Coasting Arc #2 (Orbit 37)
---------------------------------------
Vector Time (GMT): 2011/164/19:49:13
933
Vector Time (MET): N/A
Weight (LBS) : 919843
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5652971
57 A = 6746267
43 meter
Y = 2479499
46 meter E =
0007131
Z = -2723638
22 I = 51
66571
XDOT = -4186
181440 Wp = 230
04793
YDOT = -3853
565540 meter/sec RA = 176
73632 deg
ZDOT = 5166
957004 TA = 98
97917
MA = 98
89845
Ha = 199
989 n
mi
Hp = 194
722
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18546494
66 X = -5667046
63
Y = 8134840
75 feet Y = 2416206
29 meter
Z = -8935820
92 Z = -2751134
30
XDOT = -13734
191076 XDOT = -4167
879323
YDOT = -12642
931563 feet/sec YDOT = -3900
276559 meter/sec
ZDOT = 16951
958674 ZDOT = 5146
664144
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15004525
66 X = 4573379
42
Y = -13527978
37 feet Y = -4123327
81 meter
Z = -9047375
58 Z = -2757640
08
XDOT = 16118
222649 XDOT = 4912
834263
YDOT = 6566
047884 feet/sec YDOT = 2001
331395 meter/sec
ZDOT = 16869
834859 ZDOT = 5141
925665
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 11164
83142890
00016717 00000-0 10270-3 0 9016
2 25544 51
6405 177
7900 0011866 233
2292 126
7780 15
67915474 380
Satellite: ISS
Catalog Number: 25544
Epoch time: 11164
83142890 = yrday
fracday
Element set: 901
Inclination: 51
6405 deg
RA of node: 177
7900 deg
Eccentricity:
0011866
Arg of perigee: 233
2292 deg
Mean anomaly: 126
7780 deg
Mean motion: 15
67915474 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 38
Checksum: 310
Coasting Arc #3 (Orbit 53)
---------------------------------------
Vector Time (GMT): 2011/165/19:49:13
933
Vector Time (MET): N/A
Weight (LBS) : 919843
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5671956
07 A = 6745221
21 meter
Y = 1728733
07 meter E =
0009254
Z = -3202225
37 I = 51
69223
XDOT = -4062
544488 Wp = 218
03757
YDOT = 4428
692326 meter/sec RA = 171
69720 deg
ZDOT = -4804
753694 TA = 359
23170
MA = 359
23312
Ha = 199
864 n
mi
Hp = 194
958
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18608779
75 X = 5667759
36
Y = 5671696
42 feet Y = 1792137
49 meter
Z = -10505988
76 Z = -3174680
78
XDOT = -13328
558033 XDOT = -4088
424352
YDOT = 14529
830467 feet/sec YDOT = 4383
118723 meter/sec
ZDOT = -15763
627604 ZDOT = -4824
551593
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19496884
93 X = -5942650
53
Y = 811831
01 feet Y = 247446
09 meter
Z = -10394375
03 Z = -3168205
51
XDOT = 7753
510891 XDOT = 2363
270120
YDOT = -16662
004926 feet/sec YDOT = -5078
579101 meter/sec
ZDOT = -15844
062040 ZDOT = -4829
270110
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 11165
85120599
00016717 00000-0 10270-3 0 9022
2 25544 51
6404 172
6002 0012011 237
5312 122
4688 15
67911874 547
Satellite: ISS
Catalog Number: 25544
Epoch time: 11165
85120599 = yrday
fracday
Element set: 902
Inclination: 51
6404 deg
RA of node: 172
6002 deg
Eccentricity:
0012011
Arg of perigee: 237
5312 deg
Mean anomaly: 122
4688 deg
Mean motion: 15
67911874 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 54
Checksum: 283
Coasting Arc #4 (Orbit 66)
---------------------------------------
Vector Time (GMT): 2011/166/15:20:34
915
Vector Time (MET): N/A
Weight (LBS) : 918520
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3713453
03 A = 6750384
12 meter
Y = -4015380
58 meter E =
0009566
Z = 3947671
62 I = 51
70490
XDOT = 6288
164277 Wp = 95
81395
YDOT = 1857
119358 meter/sec RA = 167
50858 deg
ZDOT = -4018
734266 TA = 35
96537
MA = 35
90103
Ha = 203
456 n
mi
Hp = 197
671
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12183244
86 X = 3738900
76
Y = -13173820
79 feet Y = -3973712
99 meter
Z = 12951678
55 Z = 3965772
56
XDOT = 20630
460227 XDOT = 6286
452509
YDOT = 6092
911280 feet/sec YDOT = 1927
428664 meter/sec
ZDOT = -13184
823708 ZDOT = -3988
190190
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17890200
07 X = -5452932
98
Y = 105522
59 feet Y = 32163
29 meter
Z = 13025229
10 Z = 3970089
83
XDOT = -9633
032894 XDOT = -2936
148426
YDOT = -18009
790572 feet/sec YDOT = -5489
384166 meter/sec
ZDOT = -13061
038389 ZDOT = -3981
004501
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 11166
67986859
00016717 00000-0 10270-3 0 9033
2 25544 51
6366 168
3818 0003234 202
7877 157
3138 15
65257511 678
Satellite: ISS
Catalog Number: 25544
Epoch time: 11166
67986859 = yrday
fracday
Element set: 903
Inclination: 51
6366 deg
RA of node: 168
3818 deg
Eccentricity:
0003234
Arg of perigee: 202
7877 deg
Mean anomaly: 157
3138 deg
Mean motion: 15
65257511 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 67
Checksum: 335
Coasting Arc #5 (Orbit 69)
---------------------------------------
Vector Time (GMT): 2011/166/19:27:28
135
Vector Time (MET): N/A
Weight (LBS) : 916899
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6546466
40 A = 6765517
36 meter
Y = 195376
05 meter E =
0009530
Z = 1670543
75 I = 51
73097
XDOT = 1312
890425 Wp = 15
77211
YDOT = -4952
239719 meter/sec RA = 166
68238 deg
ZDOT = 5725
420265 TA = 2
57683
MA = 2
57193
Ha = 207
725 n
mi
Hp = 205
311
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21477908
15 X = -6556279
76
Y = 640997
55 feet Y = 122114
29 meter
Z = 5480786
59 Z = 1638717
29
XDOT = 4307
383283 XDOT = 1340
356763
YDOT = -16247
505641 feet/sec YDOT = -4937
405758 meter/sec
ZDOT = 18784
187220 ZDOT = 5731
863994
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20631946
62 X = 6288617
33
Y = -6118194
76 feet Y = -1864825
76 meter
Z = 5351720
20 Z = 1631204
32
XDOT = -348
589015 XDOT = -106
249932
YDOT = 15274
531665 feet/sec YDOT = 4655
677251 meter/sec
ZDOT = 18810
504535 ZDOT = 5733
441782
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 11166
87154009
00016717 00000-0 10270-3 0 9040
2 25544 51
6389 167
4129 0010420 286
6121 73
3891 15
61961786 705
Satellite: ISS
Catalog Number: 25544
Epoch time: 11166
87154009 = yrday
fracday
Element set: 904
Inclination: 51
6389 deg
RA of node: 167
4129 deg
Eccentricity:
0010420
Arg of perigee: 286
6121 deg
Mean anomaly: 73
3891 deg
Mean motion: 15
61961786 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 70
Checksum: 309
Coasting Arc #6 (Orbit 84)
---------------------------------------
Vector Time (GMT): 2011/167/19:27:28
135
Vector Time (MET): N/A
Weight (LBS) : 916899
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3890933
12 A = 6756683
20 meter
Y = 2712131
58 meter E =
0007281
Z = -4816061
17 I = 51
73126
XDOT = -5987
033320 Wp = 8
69252
YDOT = 4087
538497 meter/sec RA = 161
64875 deg
ZDOT = -2528
558412 TA = 236
47086
MA = 236
54044
Ha = 207
901 n
mi
Hp = 205
114
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12765528
61 X = 3883711
73
Y = 8898069
48 feet Y = 2755602
92 meter
Z = -15800725
64 Z = -4797176
17
XDOT = -19642
497770 XDOT = -6020
012808
YDOT = 13410
559374 feet/sec YDOT = 4020
403953 meter/sec
ZDOT = -8295
795314 ZDOT = -2557
722510
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14796416
10 X = -4509947
63
Y = -5060803
56 feet Y = -1542532
92 meter
Z = -15724237
02 Z = -4792747
44
XDOT = 14833
261373 XDOT = 4521
178066
YDOT = -17157
852886 feet/sec YDOT = -5229
713560 meter/sec
ZDOT = -8414
232867 ZDOT = -2564
658178
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 11167
83121582
00016717 00000-0 10270-3 0 9058
2 25544 51
6392 162
5718 0010529 290
1311 69
8713 15
62009616 855
Satellite: ISS
Catalog Number: 25544
Epoch time: 11167
83121582 = yrday
fracday
Element set: 905
Inclination: 51
6392 deg
RA of node: 162
5718 deg
Eccentricity:
0010529
Arg of perigee: 290
1311 deg
Mean anomaly: 69
8713 deg
Mean motion: 15
62009616 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 85
Checksum: 297
Coasting Arc #7 (Orbit 100)
---------------------------------------
Vector Time (GMT): 2011/168/19:27:28
135
Vector Time (MET): N/A
Weight (LBS) : 916899
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 805103
88 A = 6756033
98 meter
Y = -4570895
88 meter E =
0008804
Z = 4915757
02 I = 51
75853
XDOT = 7235
099506 Wp = 331
77349
YDOT = -1179
814456 meter/sec RA = 156
57461 deg
ZDOT = -2276
088686 TA = 140
44014
MA = 140
37585
Ha = 208
038 n
mi
Hp = 204
856
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2641416
94 X = 832277
10
Y = -14996377
56 feet Y = -4561741
69 meter
Z = 16127811
75 Z = 4919733
34
XDOT = 23737
203105 XDOT = 7258
811388
YDOT = -3870
782337 feet/sec YDOT = -1098
774182 meter/sec
ZDOT = -7467
482565 ZDOT = -2240
883587
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1893222
43 X = 577054
20
Y = 15091651
87 feet Y = 4599935
49 meter
Z = 16144116
20 Z = 4920726
62
XDOT = -20550
753385 XDOT = -6263
869632
YDOT = 10434
265969 feet/sec YDOT = 3180
364267 meter/sec
ZDOT = -7324
634566 ZDOT = -2232
548616
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 11168
85485774
00016717 00000-0 10270-3 0 9068
2 25544 51
6396 157
4075 0010612 293
8310 66
1734 15
62052446 1011
Satellite: ISS
Catalog Number: 25544
Epoch time: 11168
85485774 = yrday
fracday
Element set: 906
Inclination: 51
6396 deg
RA of node: 157
4075 deg
Eccentricity:
0010612
Arg of perigee: 293
8310 deg
Mean anomaly: 66
1734 deg
Mean motion: 15
62052446 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 101
Checksum: 303
Coasting Arc #8 (Orbit 115)
---------------------------------------
Vector Time (GMT): 2011/169/19:27:28
135
Vector Time (MET): N/A
Weight (LBS) : 916899
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4845003
38 A = 6764887
85 meter
Y = 4315162
51 meter E =
0011499
Z = -1887901
70 I = 51
81527
XDOT = -4518
108408 Wp = 334
60600
YDOT = -2601
705736 meter/sec RA = 151
54005 deg
ZDOT = 5645
798492 TA = 4
57278
MA = 4
56228
Ha = 208
313 n
mi
Hp = 204
704
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15895680
39 X = -4883725
31
Y = 14157357
30 feet Y = 4260766
54 meter
Z = -6193903
20 Z = -1911531
76
XDOT = -14823
190316 XDOT = -4516
105731
YDOT = -8535
779974 feet/sec YDOT = -2652
219694 meter/sec
ZDOT = 18522
960932 ZDOT = 5623
854253
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10782045
05 X = 3286367
33
Y = -18320811
06 feet Y = -5584183
21 meter
Z = -6289931
98 Z = -1917171
27
XDOT = 15490
249765 XDOT = 4721
428128
YDOT = 2784
623025 feet/sec YDOT = 848
753098 meter/sec
ZDOT = 18434
036680 ZDOT = 5618
694380
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 11169
81451190
00016717 00000-0 10270-3 0 9071
2 25544 51
6395 152
5655 0010637 297
6149 62
3927 15
62028472 1169
Satellite: ISS
Catalog Number: 25544
Epoch time: 11169
81451190 = yrday
fracday
Element set: 907
Inclination: 51
6395 deg
RA of node: 152
5655 deg
Eccentricity:
0010637
Arg of perigee: 297
6149 deg
Mean anomaly: 62
3927 deg
Mean motion: 15
62028472 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 116
Checksum: 314
Coasting Arc #9 (Orbit 131)
---------------------------------------
Vector Time (GMT): 2011/170/19:27:28
135
Vector Time (MET): N/A
Weight (LBS) : 916899
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6080040
85 A = 6764171
91 meter
Y = -1803806
54 meter E =
0005249
Z = -2350190
39 I = 51
83858
XDOT = -488
464864 Wp = 284
22500
YDOT = 5421
747669 meter/sec RA = 146
54509 deg
ZDOT = -5413
610209 TA = 282
00267
MA = 282
06150
Ha = 208
523 n
mi
Hp = 204
668
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19947640
59 X = 6111176
12
Y = -5918000
47 feet Y = -1735641
41 meter
Z = -7710598
38 Z = -2320578
58
XDOT = -1602
575013 XDOT = -522
757612
YDOT = 17787
886053 feet/sec YDOT = 5416
094382 meter/sec
ZDOT = -17761
188351 ZDOT = -5416
065669
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17029694
30 X = -5190650
82
Y = 12031624
14 feet Y = 3667239
04 meter
Z = -7590385
69 Z = -2313549
56
XDOT = -3424
210466 XDOT = -1043
699350
YDOT = -16081
922569 feet/sec YDOT = -4901
769999 meter/sec
ZDOT = -17771
359377 ZDOT = -5416
710338
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 11170
83812955
00016717 00000-0 10270-3 0 9086
2 25544 51
6393 147
4018 0010643 300
4908 59
5197 15
62027944 1324
Satellite: ISS
Catalog Number: 25544
Epoch time: 11170
83812955 = yrday
fracday
Element set: 908
Inclination: 51
6393 deg
RA of node: 147
4018 deg
Eccentricity:
0010643
Arg of perigee: 300
4908 deg
Mean anomaly: 59
5197 deg
Mean motion: 15
62027944 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 132
Checksum: 304
Coasting Arc #10 (Orbit 147)
---------------------------------------
Vector Time (GMT): 2011/171/19:27:28
135
Vector Time (MET): N/A
Weight (LBS) : 916899
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3995334
25 A = 6755392
39 meter
Y = -1937884
32 meter E =
0005278
Z = 5093797
13 I = 51
83401
XDOT = 4920
816499 Wp = 305
65895
YDOT = -5639
028698 meter/sec RA = 141
50684 deg
ZDOT = 1718
592857 TA = 127
82653
MA = 127
77875
Ha = 208
816 n
mi
Hp = 204
352
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13108052
01 X = -3998111
95
Y = -6357888
17 feet Y = -1982578
72 meter
Z = 16711932
85 Z = 5074381
05
XDOT = 16144
411086 XDOT = 4975
158968
YDOT = -18500
750323 feet/sec YDOT = -5583
697502 meter/sec
ZDOT = 5638
428010 ZDOT = 1742
629203
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14579052
89 X = 4443695
32
Y = 1523002
30 feet Y = 464211
10 meter
Z = 16633224
28 Z = 5069806
76
XDOT = -8804
828046 XDOT = -2683
711588
YDOT = 21791
087590 feet/sec YDOT = 6641
923497 meter/sec
ZDOT = 5736
177636 ZDOT = 1748
386943
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 11171
86173405
00016717 00000-0 10270-3 0 9091
2 25544 51
6393 142
2366 0010569 305
3517 54
6651 15
62049147 1487
Satellite: ISS
Catalog Number: 25544
Epoch time: 11171
86173405 = yrday
fracday
Element set: 909
Inclination: 51
6393 deg
RA of node: 142
2366 deg
Eccentricity:
0010569
Arg of perigee: 305
3517 deg
Mean anomaly: 54
6651 deg
Mean motion: 15
62049147 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 148
Checksum: 302
Coasting Arc #11 (Orbit 162)
---------------------------------------
Vector Time (GMT): 2011/172/19:27:28
135
Vector Time (MET): N/A
Weight (LBS) : 916899
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -16913
45 A = 6757276
87 meter
Y = 4972685
72 meter E =
0003322
Z = -4574691
74 I = 51
86299
XDOT = -6454
671313 Wp = 20
94221
YDOT = 2804
885485 meter/sec RA = 136
43956 deg
ZDOT = 3076
487390 TA = 279
65275
MA = 279
69028
Ha = 208
875 n
mi
Hp = 204
015
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -55490
33 X = -50294
92
Y = 16314585
70 feet Y = 4972310
44 meter
Z = -15008831
18 Z = -4574854
45
XDOT = -21176
743152 XDOT = -6500
501231
YDOT = 9202
380200 feet/sec YDOT = 2732
448841 meter/sec
ZDOT = 10093
462566 ZDOT = 3045
019881
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5805143
91 X = -1769407
86
Y = -15246094
67 feet Y = -4647009
66 meter
Z = -15009686
88 Z = -4574952
56
XDOT = 15494
706999 XDOT = 4722
786693
YDOT = -15698
935747 feet/sec YDOT = -4785
035616 meter/sec
ZDOT = 9965
658093 ZDOT = 3037
532587
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 11172
82134918
00016717 00000-0 10270-3 0 9106
2 25544 51
6383 137
3941 0010668 308
2940 51
7257 15
62102183 1639
Satellite: ISS
Catalog Number: 25544
Epoch time: 11172
82134918 = yrday
fracday
Element set: 910
Inclination: 51
6383 deg
RA of node: 137
3941 deg
Eccentricity:
0010668
Arg of perigee: 308
2940 deg
Mean anomaly: 51
7257 deg
Mean motion: 15
62102183 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 163
Checksum: 289
Coasting Arc #12 (Orbit 178)
---------------------------------------
Vector Time (GMT): 2011/173/19:27:28
135
Vector Time (MET): N/A
Weight (LBS) : 916899
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3726101
48 A = 6765619
72 meter
Y = -5536380
18 meter E =
0003654
Z = 1108784
40 I = 51
91255
XDOT = 4531
983330 Wp = 93
33623
YDOT = 1863
413585 meter/sec RA = 131
42357 deg
ZDOT = -5908
963425 TA = 74
64443
MA = 74
60405
Ha = 209
031 n
mi
Hp = 203
744
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12224742
39 X = 3782347
18
Y = -18163976
97 feet Y = -5494398
28 meter
Z = 3637744
10 Z = 1127021
73
XDOT = 14868
711712 XDOT = 4539
513942
YDOT = 6113
561629 feet/sec YDOT = 1914
135706 meter/sec
ZDOT = -19386
362943 ZDOT = -5886
928699
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4618574
81 X = -1407741
60
Y = 21389192
44 feet Y = 6519425
86 meter
Z = 3711978
11 Z = 1131410
93
XDOT = -14623
350203 XDOT = -4457
197142
YDOT = 200
475636 feet/sec YDOT = 61
104974 meter/sec
ZDOT = -19297
015356 ZDOT = -5881
730280
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
84492645
00016717 00000-0 10270-3 0 9114
2 25544 51
6385 132
2302 0010710 312
5333 47
4918 15
62129437 1792
Satellite: ISS
Catalog Number: 25544
Epoch time: 11173
84492645 = yrday
fracday
Element set: 911
Inclination: 51
6385 deg
RA of node: 132
2302 deg
Eccentricity:
0010710
Arg of perigee: 312
5333 deg
Mean anomaly: 47
4918 deg
Mean motion: 15
62129437 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 179
Checksum: 290
Coasting Arc #13 (Orbit 194)
---------------------------------------
Vector Time (GMT): 2011/174/19:27:28
135
Vector Time (MET): N/A
Weight (LBS) : 916899
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5211300
06 A = 6762139
05 meter
Y = 3001443
05 meter E =
0010500
Z = 3076433
39 I = 51
91892
XDOT = -470
530677 Wp = 31
64036
YDOT = -5873
577852 meter/sec RA = 126
42952 deg
ZDOT = 4934
498893 TA = 3
71075
MA = 3
70297
Ha = 209
248 n
mi
Hp = 203
547
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17097441
13 X = -5259420
17
Y = 9847254
09 feet Y = 2942897
73 meter
Z = 10093285
41 Z = 3051000
42
XDOT = -1543
735816 XDOT = -428
787051
YDOT = -19270
268543 feet/sec YDOT = -5878
606750 meter/sec
ZDOT = 16189
300830 ZDOT = 4932
313815
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12029879
33 X = 3666707
22
Y = -15705043
51 feet Y = -4786897
26 meter
Z = 9989941
37 Z = 3044934
13
XDOT = 7803
164430 XDOT = 2378
404518
YDOT = 16267
206884 feet/sec YDOT = 4958
244658 meter/sec
ZDOT = 16180
675636 ZDOT = 4931
869934
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
86848919
00016717 00000-0 10270-3 0 9127
2 25544 51
6372 127
0641 0010725 315
2627 44
7664 15
62149267 1957
Satellite: ISS
Catalog Number: 25544
Epoch time: 11174
86848919 = yrday
fracday
Element set: 912
Inclination: 51
6372 deg
RA of node: 127
0641 deg
Eccentricity:
0010725
Arg of perigee: 315
2627 deg
Mean anomaly: 44
7664 deg
Mean motion: 15
62149267 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 195
Checksum: 318
Coasting Arc #14 (Orbit 209)
---------------------------------------
Vector Time (GMT): 2011/175/19:27:28
135
Vector Time (MET): N/A
Weight (LBS) : 916899
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3980022
89 A = 6754284
04 meter
Y = 1418630
48 meter E =
0012257
Z = -5277105
67 I = 51
90862
XDOT = -3453
199276 Wp = 38
80157
YDOT = 6811
812325 meter/sec RA = 121
38497 deg
ZDOT = -764
860305 TA = 223
87550
MA = 223
97291
Ha = 209
365 n
mi
Hp = 203
391
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13057817
88 X = 3989498
90
Y = 4654299
47 feet Y = 1463191
12 meter
Z = -17313338
80 Z = -5257747
54
XDOT = -11329
393949 XDOT = -3525
398074
YDOT = 22348
465634 feet/sec YDOT = 6772
792957 meter/sec
ZDOT = -2509
384203 ZDOT = -781
810502
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13922355
90 X = -4243534
08
Y = 1024435
08 feet Y = 312247
81 meter
Z = -17234829
58 Z = -5253176
06
XDOT = 1460
427625 XDOT = 445
138340
YDOT = -23995
510200 feet/sec YDOT = -7313
831509 meter/sec
ZDOT = -2578
473031 ZDOT = -785
918580
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
82806781
00016717 00000-0 10270-3 0 9136
2 25544 51
6360 122
2214 0010585 319
4051 40
6316 15
62157077 2103
Satellite: ISS
Catalog Number: 25544
Epoch time: 11175
82806781 = yrday
fracday
Element set: 913
Inclination: 51
6360 deg
RA of node: 122
2214 deg
Eccentricity:
0010585
Arg of perigee: 319
4051 deg
Mean anomaly: 40
6316 deg
Mean motion: 15
62157077 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 210
Checksum: 273
Coasting Arc #15 (Orbit 225)
---------------------------------------
Vector Time (GMT): 2011/176/19:27:28
135
Vector Time (MET): N/A
Weight (LBS) : 916899
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -902170
55 A = 6759001
63 meter
Y = -5335223
18 meter E =
0011453
Z = 4054794
47 I = 51
94024
XDOT = 5340
417203 Wp = 20
34423
YDOT = -3886
505099 meter/sec RA = 116
32747 deg
ZDOT = -3911
798975 TA = 110
04853
MA = 109
92521
Ha = 209
428 n
mi
Hp = 203
109
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2959877
14 X = -862141
49
Y = -17504013
05 feet Y = -5345088
52 meter
Z = 13303131
47 Z = 4050508
24
XDOT = 17521
053814 XDOT = 5402
482773
YDOT = -12751
000982 feet/sec YDOT = -3826
437759 meter/sec
ZDOT = -12833
986137 ZDOT = -3885
704951
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10066942
00 X = 3068403
92
Y = 14637769
43 feet Y = 4461592
12 meter
Z = 13285971
45 Z = 4049564
10
XDOT = -9603
199429 XDOT = -2927
055186
YDOT = 18198
034558 feet/sec YDOT = 5546
760933 meter/sec
ZDOT = -12727
896243 ZDOT = -3879
462775
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
85160286
00016717 00000-0 10270-3 0 9144
2 25544 51
6367 117
0562 0010680 322
4575 37
5835 15
62183217 2262
Satellite: ISS
Catalog Number: 25544
Epoch time: 11176
85160286 = yrday
fracday
Element set: 914
Inclination: 51
6367 deg
RA of node: 117
0562 deg
Eccentricity:
0010680
Arg of perigee: 322
4575 deg
Mean anomaly: 37
5835 deg
Mean motion: 15
62183217 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 226
Checksum: 300
Coasting Arc #16 (Orbit 240)
---------------------------------------
Vector Time (GMT): 2011/177/19:27:28
135
Vector Time (MET): N/A
Weight (LBS) : 916899
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2309155
65 A = 6765997
16 meter
Y = 6344251
00 meter E =
0017432
Z = -199597
29 I = 51
97543
XDOT = -4512
925040 Wp = 7
62042
YDOT = -1454
595596 meter/sec RA = 111
32499 deg
ZDOT = 6052
499840 TA = 350
22973
MA = 350
26358
Ha = 209
595 n
mi
Hp = 202
835
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7575969
98 X = -2378957
06
Y = 20814471
79 feet Y = 6318038
37 meter
Z = -654846
74 Z = -210983
78
XDOT = -14806
184516 XDOT = -4525
726055
YDOT = -4772
295261 feet/sec YDOT = -1505
134348 meter/sec
ZDOT = 19857
282941 ZDOT = 6030
544698
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2184791
09 X = -665924
32
Y = -22040897
42 feet Y = -6718065
53 meter
Z = -701363
06 Z = -213775
46
XDOT = 13912
464059 XDOT = 4240
519045
YDOT = -2000
619961 feet/sec YDOT = -609
788964 meter/sec
ZDOT = 19768
227220 ZDOT = 6025
355657
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
81115560
00016717 00000-0 10270-3 0 9157
2 25544 51
6360 112
2129 0010545 326
4305 33
6183 15
62185098 2415
Satellite: ISS
Catalog Number: 25544
Epoch time: 11177
81115560 = yrday
fracday
Element set: 915
Inclination: 51
6360 deg
RA of node: 112
2129 deg
Eccentricity:
0010545
Arg of perigee: 326
4305 deg
Mean anomaly: 33
6183 deg
Mean motion: 15
62185098 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 241
Checksum: 276
Coasting Arc #17 (Orbit 255)
---------------------------------------
Vector Time (GMT): 2011/178/19:27:28
135
Vector Time (MET): N/A
Weight (LBS) : 916899
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4186255
93 A = 6759775
41 meter
Y = -3714612
26 meter E =
0010585
Z = -3800562
82 I = 51
96533
XDOT = 1637
947963 Wp = 4
32772
YDOT = 6186
484127 meter/sec RA = 106
32891 deg
ZDOT = -4232
878748 TA = 221
17244
MA = 221
25234
Ha = 209
689 n
mi
Hp = 202
615
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13734435
46 X = 4245944
76
Y = -12187048
10 feet Y = -3667464
63 meter
Z = -12469038
13 Z = -3780081
62
XDOT = 5373
845023 XDOT = 1589
210334
YDOT = 20296
863933 feet/sec YDOT = 6204
528859 meter/sec
ZDOT = -13887
397467 ZDOT = -4225
038938
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6879296
85 X = -2096809
68
Y = 17085233
14 feet Y = 5207579
06 meter
Z = -12385711
69 Z = -3775164
92
XDOT = -12731
601380 XDOT = -3880
592101
YDOT = -15193
758820 feet/sec YDOT = -4631
057688 meter/sec
ZDOT = -13855
869571 ZDOT = -4223
269045
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
83466400
00016717 00000-0 10270-3 0 9163
2 25544 51
6363 107
0481 0010484 331
0970 28
9605 15
62234564 2568
Satellite: ISS
Catalog Number: 25544
Epoch time: 11178
83466400 = yrday
fracday
Element set: 916
Inclination: 51
6363 deg
RA of node: 107
0481 deg
Eccentricity:
0010484
Arg of perigee: 331
0970 deg
Mean anomaly: 28
9605 deg
Mean motion: 15
62234564 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 256
Checksum: 295
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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