[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
June 9th 2012
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) : 130 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
172/13:49:37
930 -0
8 4
2 4
2
N/A 4
1 0
0 221
1
000/00:09:15
860 -0
4 -0
2 209
7
Coasting Arc #1 (Orbit 1665)
---------------------------------------
Vector Time (GMT): 2012/160/12:16:42
072
Vector Time (MET): N/A
Weight (LBS) : 923792
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2829761
17 A = 6775173
49 meter
Y = 4348358
54 meter E =
0016185
Z = -4368005
04 I = 51
71573
XDOT = -6776
376169 Wp = 73
29779
YDOT = -965
034312 meter/sec RA = 164
70224 deg
ZDOT = 3444
401074 TA = 231
56581
MA = 231
71120
Ha = 221
234 n
mi
Hp = 208
292
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9283993
35 X = -2856956
43
Y = 14266268
18 feet Y = 4316562
90 meter
Z = -14330725
19 Z = -4381817
32
XDOT = -22232
205279 XDOT = -6781
813345
YDOT = -3166
123070 feet/sec YDOT = -1040
842785 meter/sec
ZDOT = 11300
528458 ZDOT = 3411
468601
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12583240
58 X = 3835371
73
Y = 11390222
80 feet Y = 3471739
91 meter
Z = -14387963
92 Z = -4385451
40
XDOT = -5912
970937 XDOT = -1802
273542
YDOT = 20573
444851 feet/sec YDOT = 6270
785991 meter/sec
ZDOT = 11165
003494 ZDOT = 3403
093065
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 12160
52151563
00016717 00000-0 10270-3 0 9005
2 25544 51
6352 165
7437 0010629 41
9750 318
2216 15
56191750 16663
Satellite: ISS
Catalog Number: 25544
Epoch time: 12160
52151563 = yrday
fracday
Element set: 900
Inclination: 51
6352 deg
RA of node: 165
7437 deg
Eccentricity:
0010629
Arg of perigee: 41
9750 deg
Mean anomaly: 318
2216 deg
Mean motion: 15
56191750 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1666
Checksum: 292
Coasting Arc #2 (Orbit 1681)
---------------------------------------
Vector Time (GMT): 2012/161/12:16:42
072
Vector Time (MET): N/A
Weight (LBS) : 923792
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4882030
10 A = 6780306
93 meter
Y = -3947067
02 meter E =
0021318
Z = 2549627
63 I = 51
76206
XDOT = 4904
055495 Wp = 78
60131
YDOT = 2625
844771 meter/sec RA = 159
70900 deg
ZDOT = -5283
742031 TA = 72
77491
MA = 72
54170
Ha = 221
194 n
mi
Hp = 208
086
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16017159
14 X = 4913418
71
Y = -12949694
95 feet Y = -3892297
91 meter
Z = 8364920
03 Z = 2573420
02
XDOT = 16089
420914 XDOT = 4899
995381
YDOT = 8614
976282 feet/sec YDOT = 2680
662823 meter/sec
ZDOT = -17335
111651 ZDOT = -5259
928041
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10491250
59 X = -3197733
18
Y = -17678327
38 feet Y = -5388354
18 meter
Z = 8463230
79 Z = 2579592
75
XDOT = 9586
975586 XDOT = 2922
110159
YDOT = -14005
904679 feet/sec YDOT = -4268
999746 meter/sec
ZDOT = -17237
262082 ZDOT = -5253
917482
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 12161
54895979
00016717 00000-0 10270-3 0 9015
2 25544 51
6345 160
6037 0010694 45
3161 314
8862 15
56263503 16824
Satellite: ISS
Catalog Number: 25544
Epoch time: 12161
54895979 = yrday
fracday
Element set: 901
Inclination: 51
6345 deg
RA of node: 160
6037 deg
Eccentricity:
0010694
Arg of perigee: 45
3161 deg
Mean anomaly: 314
8862 deg
Mean motion: 15
56263503 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1682
Checksum: 313
Coasting Arc #3 (Orbit 1696)
---------------------------------------
Vector Time (GMT): 2012/162/12:16:42
072
Vector Time (MET): N/A
Weight (LBS) : 923792
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6030126
43 A = 6782980
89 meter
Y = 3073526
19 meter E =
0022043
Z = -261725
04 I = 51
79941
XDOT = -2353
592633 Wp = 46
88754
YDOT = -4132
909681 meter/sec RA = 154
73610 deg
ZDOT = 6025
993191 TA = 310
29405
MA = 310
48651
Ha = 221
165 n
mi
Hp = 207
953
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19783879
38 X = -6062775
66
Y = 10083747
35 feet Y = 3005911
06 meter
Z = -858677
96 Z = -291098
07
XDOT = -7721
760606 XDOT = -2336
475509
YDOT = -13559
414963 feet/sec YDOT = -4159
133868 meter/sec
ZDOT = 19770
318869 ZDOT = 6014
600761
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7462885
20 X = 2274687
41
Y = 20908522
02 feet Y = 6372917
51 meter
Z = -979909
71 Z = -298676
48
XDOT = -12927
548252 XDOT = -3940
316707
YDOT = 5493
675118 feet/sec YDOT = 1674
472176 meter/sec
ZDOT = 19723
745924 ZDOT = 6011
797758
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 12162
51217537
00016717 00000-0 10270-3 0 9022
2 25544 51
6344 155
7868 0010574 50
2575 309
9508 15
56302882 16973
Satellite: ISS
Catalog Number: 25544
Epoch time: 12162
51217537 = yrday
fracday
Element set: 902
Inclination: 51
6344 deg
RA of node: 155
7868 deg
Eccentricity:
0010574
Arg of perigee: 50
2575 deg
Mean anomaly: 309
9508 deg
Mean motion: 15
56302882 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1697
Checksum: 319
Coasting Arc #4 (Orbit 1712)
---------------------------------------
Vector Time (GMT): 2012/163/12:16:42
072
Vector Time (MET): N/A
Weight (LBS) : 923792
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6216254
12 A = 6781152
87 meter
Y = -1662752
69 meter E =
0012877
Z = -2153709
34 I = 51
82003
XDOT = -483
274259 Wp = 82
76445
YDOT = 5299
071888 meter/sec RA = 149
76531 deg
ZDOT = -5512
626956 TA = 121
04956
MA = 120
92307
Ha = 221
317 n
mi
Hp = 207
915
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20394534
52 X = 6244847
59
Y = -5455225
37 feet Y = -1593078
62 meter
Z = -7065975
51 Z = -2123441
72
XDOT = -1585
545470 XDOT = -515
714532
YDOT = 17385
406457 feet/sec YDOT = 5293
486718 meter/sec
ZDOT = -18086
046443 ZDOT = -5515
053012
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3148844
40 X = -959767
77
Y = -20917206
34 feet Y = -6375564
49 meter
Z = -6941166
33 Z = -2115667
50
XDOT = 15587
017746 XDOT = 4750
923009
YDOT = 3629
158027 feet/sec YDOT = 1106
167367 meter/sec
ZDOT = -18096
487530 ZDOT = -5515
809399
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 12163
53958933
00016717 00000-0 10270-3 0 9038
2 25544 51
6342 150
6463 0010730 52
7861 307
4271 15
56286932 17131
Satellite: ISS
Catalog Number: 25544
Epoch time: 12163
53958933 = yrday
fracday
Element set: 903
Inclination: 51
6342 deg
RA of node: 150
6463 deg
Eccentricity:
0010730
Arg of perigee: 52
7861 deg
Mean anomaly: 307
4271 deg
Mean motion: 15
56286932 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1713
Checksum: 303
Coasting Arc #5 (Orbit 1728)
---------------------------------------
Vector Time (GMT): 2012/164/12:16:42
072
Vector Time (MET): N/A
Weight (LBS) : 923792
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5400870
44 A = 6775960
18 meter
Y = -105449
66 meter E =
0019523
Z = 4071543
36 I = 51
82866
XDOT = 3050
025506 Wp = 79
67938
YDOT = -5887
327134 meter/sec RA = 144
78304 deg
ZDOT = 3881
025692 TA = 330
28249
MA = 330
39325
Ha = 221
303 n
mi
Hp = 207
785
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17719391
22 X = -5419068
59
Y = -345963
44 feet Y = -165947
66 meter
Z = 13358081
88 Z = 4045261
85
XDOT = 10006
645360 XDOT = 3096
778897
YDOT = -19315
377737 feet/sec YDOT = -5852
958802 meter/sec
ZDOT = 12733
023925 ZDOT = 3895
955663
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2018725
38 X = -615307
50
Y = 17689023
83 feet Y = 5391614
46 meter
Z = 13249832
11 Z = 4038548
83
XDOT = -17004
572086 XDOT = -5182
993572
YDOT = -11555
188450 feet/sec YDOT = -3522
021440 meter/sec
ZDOT = 12795
027726 ZDOT = 3899
924451
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 12164
56698535
00016717 00000-0 10270-3 0 9042
2 25544 51
6340 145
5077 0010489 56
1725 304
0426 15
56337207 17295
Satellite: ISS
Catalog Number: 25544
Epoch time: 12164
56698535 = yrday
fracday
Element set: 904
Inclination: 51
6340 deg
RA of node: 145
5077 deg
Eccentricity:
0010489
Arg of perigee: 56
1725 deg
Mean anomaly: 304
0426 deg
Mean motion: 15
56337207 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1729
Checksum: 311
Coasting Arc #6 (Orbit 1743)
---------------------------------------
Vector Time (GMT): 2012/165/12:16:42
072
Vector Time (MET): N/A
Weight (LBS) : 923792
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3843379
32 A = 6771679
48 meter
Y = 2090827
30 meter E =
0024113
Z = -5189690
26 I = 51
83850
XDOT = -4970
941943 Wp = 70
94303
YDOT = 5648
086013 meter/sec RA = 139
78067 deg
ZDOT = -1403
529459 TA = 185
55671
MA = 185
58351
Ha = 221
300 n
mi
Hp = 207
763
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12609512
19 X = 3844924
11
Y = 6859669
61 feet Y = 2133815
51 meter
Z = -17026542
86 Z = -5171015
21
XDOT = -16308
864642 XDOT = -5026
912468
YDOT = 18530
465922 feet/sec YDOT = 5592
185056 meter/sec
ZDOT = -4604
755444 ZDOT = -1427
813607
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7816731
37 X = 2382539
72
Y = -12147480
35 feet Y = -3702552
01 meter
Z = -16949792
28 Z = -5166296
69
XDOT = 16336
318887 XDOT = 4979
309997
YDOT = 17088
410092 feet/sec YDOT = 5208
547396 meter/sec
ZDOT = -4705
286090 ZDOT = -1434
171200
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 12165
53015654
00016717 00000-0 10270-3 0 9056
2 25544 51
6340 140
6885 0010647 59
6663 300
5542 15
56319125 17449
Satellite: ISS
Catalog Number: 25544
Epoch time: 12165
53015654 = yrday
fracday
Element set: 905
Inclination: 51
6340 deg
RA of node: 140
6885 deg
Eccentricity:
0010647
Arg of perigee: 59
6663 deg
Mean anomaly: 300
5542 deg
Mean motion: 15
56319125 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1744
Checksum: 299
Coasting Arc #7 (Orbit 1759)
---------------------------------------
Vector Time (GMT): 2012/166/12:16:42
072
Vector Time (MET): N/A
Weight (LBS) : 923792
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1801964
86 A = 6771465
17 meter
Y = -3958787
86 meter E =
0014908
Z = 5180006
20 I = 51
86092
XDOT = 6032
438997 Wp = 60
89873
YDOT = -4552
550337 meter/sec RA = 134
77146 deg
ZDOT = -1370
711922 TA = 42
27324
MA = 42
15842
Ha = 221
325 n
mi
Hp = 207
564
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5911958
21 X = -1782726
46
Y = -12988149
15 feet Y = -3978831
58 meter
Z = 16994771
00 Z = 5171298
53
XDOT = 19791
466526 XDOT = 6089
556860
YDOT = -14936
188770 feet/sec YDOT = -4484
772345 meter/sec
ZDOT = -4497
086359 ZDOT = -1341
268157
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13323571
22 X = -4061024
51
Y = 5227991
58 feet Y = 1593491
83 meter
Z = 16959247
14 Z = 5169178
53
XDOT = -13343
240262 XDOT = -4067
019632
YDOT = -19704
759702 feet/sec YDOT = -6006
010757 meter/sec
ZDOT = -4375
378342 ZDOT = -1333
615319
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 12166
55752147
00016717 00000-0 10270-3 0 9065
2 25544 51
6340 135
5491 0010608 62
9407 297
2828 15
56353224 17600
Satellite: ISS
Catalog Number: 25544
Epoch time: 12166
55752147 = yrday
fracday
Element set: 906
Inclination: 51
6340 deg
RA of node: 135
5491 deg
Eccentricity:
0010608
Arg of perigee: 62
9407 deg
Mean anomaly: 297
2828 deg
Mean motion: 15
56353224 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1760
Checksum: 309
Coasting Arc #8 (Orbit 1774)
---------------------------------------
Vector Time (GMT): 2012/167/12:16:42
072
Vector Time (MET): N/A
Weight (LBS) : 923792
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -282143
63 A = 6775649
11 meter
Y = 5384727
66 meter E =
0016888
Z = -4116204
27 I = 51
89602
XDOT = -6092
269507 Wp = 84
04372
YDOT = 2607
444828 meter/sec RA = 129
77251 deg
ZDOT = 3843
820858 TA = 225
50240
MA = 225
64056
Ha = 221
279 n
mi
Hp = 207
485
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -925668
09 X = -322340
03
Y = 17666429
33 feet Y = 5381348
35 meter
Z = -13504607
20 Z = -4117671
85
XDOT = -19987
760849 XDOT = -6139
646262
YDOT = 8554
609015 feet/sec YDOT = 2539
051890 meter/sec
ZDOT = 12610
960820 ZDOT = 3814
109901
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17613553
18 X = 5368611
01
Y = 1595566
71 feet Y = 486328
73 meter
Z = -13511140
35 Z = -4118195
58
XDOT = 7808
720540 XDOT = 2380
098021
YDOT = 19126
328039 feet/sec YDOT = 5829
704786 meter/sec
ZDOT = 12488
308667 ZDOT = 3806
436482
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 12167
52066039
00016717 00000-0 10270-3 0 9072
2 25544 51
6342 130
7308 0010606 66
1418 294
0847 15
56360790 17750
Satellite: ISS
Catalog Number: 25544
Epoch time: 12167
52066039 = yrday
fracday
Element set: 907
Inclination: 51
6342 deg
RA of node: 130
7308 deg
Eccentricity:
0010606
Arg of perigee: 66
1418 deg
Mean anomaly: 294
0847 deg
Mean motion: 15
56360790 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1775
Checksum: 306
Coasting Arc #9 (Orbit 1790)
---------------------------------------
Vector Time (GMT): 2012/168/12:16:42
072
Vector Time (MET): N/A
Weight (LBS) : 923792
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2189574
45 A = 6780795
17 meter
Y = -6051751
30 meter E =
0023068
Z = 2113505
14 I = 51
93304
XDOT = 5308
695830 Wp = 92
95767
YDOT = -32
731779 meter/sec RA = 124
79432 deg
ZDOT = -5542
675145 TA = 63
69471
MA = 63
45793
Ha = 221
227 n
mi
Hp = 207
352
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7183643
22 X = 2246816
63
Y = -19854827
11 feet Y = -6026946
38 meter
Z = 6934071
99 Z = 2124280
23
XDOT = 17416
981071 XDOT = 5335
592551
YDOT = -107
387727 feet/sec YDOT = 26
784551 meter/sec
ZDOT = -18184
629740 ZDOT = -5516
820213
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19666318
92 X = -5994294
01
Y = -7643905
16 feet Y = -2329862
29 meter
Z = 6979029
87 Z = 2127208
30
XDOT = -220
122439 XDOT = -67
093320
YDOT = -16090
535311 feet/sec YDOT = -4904
395163 meter/sec
ZDOT = -18078
087530 ZDOT = -5510
201079
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 12168
54799243
00016717 00000-0 10270-3 0 9086
2 25544 51
6349 125
5905 0010600 69
9115 290
3179 15
56407279 17910
Satellite: ISS
Catalog Number: 25544
Epoch time: 12168
54799243 = yrday
fracday
Element set: 908
Inclination: 51
6349 deg
RA of node: 125
5905 deg
Eccentricity:
0010600
Arg of perigee: 69
9115 deg
Mean anomaly: 290
3179 deg
Mean motion: 15
56407279 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1791
Checksum: 330
Coasting Arc #10 (Orbit 1806)
---------------------------------------
Vector Time (GMT): 2012/169/12:16:42
072
Vector Time (MET): N/A
Weight (LBS) : 923792
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3556973
90 A = 6782600
27 meter
Y = 5758294
87 meter E =
0022565
Z = 282421
79 I = 51
95609
XDOT = -3887
820081 Wp = 59
85405
YDOT = -2714
616626 meter/sec RA = 119
83300 deg
ZDOT = 6035
691981 TA = 303
18050
MA = 303
39671
Ha = 221
185 n
mi
Hp = 207
300
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11669861
89 X = -3622471
92
Y = 18892043
52 feet Y = 5718152
32 meter
Z = 926580
69 Z = 264983
90
XDOT = -12755
315226 XDOT = -3886
495916
YDOT = -8906
222527 feet/sec YDOT = -2758
086201 meter/sec
ZDOT = 19802
139046 ZDOT = 6016
807800
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18795313
33 X = 5728811
50
Y = 11830473
99 feet Y = 3605928
47 meter
Z = 854177
22 Z = 260353
22
XDOT = -8147
979470 XDOT = -2483
504142
YDOT = 11431
482062 feet/sec YDOT = 3484
315732 meter/sec
ZDOT = 19724
570787 ZDOT = 6012
049176
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 12169
57530673
00016717 00000-0 10270-3 0 9091
2 25544 51
6351 120
4511 0010532 73
8443 286
3869 15
56438212 18072
Satellite: ISS
Catalog Number: 25544
Epoch time: 12169
57530673 = yrday
fracday
Element set: 909
Inclination: 51
6351 deg
RA of node: 120
4511 deg
Eccentricity:
0010532
Arg of perigee: 73
8443 deg
Mean anomaly: 286
3869 deg
Mean motion: 15
56438212 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1807
Checksum: 307
Coasting Arc #11 (Orbit 1821)
---------------------------------------
Vector Time (GMT): 2012/170/12:16:42
072
Vector Time (MET): N/A
Weight (LBS) : 923792
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4377429
08 A = 6779505
86 meter
Y = -4425755
30 meter E =
0014297
Z = -2697179
42 I = 51
96155
XDOT = 2077
390708 Wp = 91
97178
YDOT = 5217
183928 meter/sec RA = 114
87002 deg
ZDOT = -5213
520954 TA = 118
34585
MA = 118
20159
Ha = 221
171 n
mi
Hp = 207
270
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14361643
95 X = 4439695
75
Y = -14520194
54 feet Y = -4376455
57 meter
Z = -8849013
84 Z = -2675763
51
XDOT = 6815
586313 XDOT = 2044
222862
YDOT = 17116
745170 feet/sec YDOT = 5240
230026 meter/sec
ZDOT = -17104
727540 ZDOT = -5203
508739
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14649443
71 X = -4465150
44
Y = -14284551
58 feet Y = -4353931
32 meter
Z = -8760325
19 Z = -2670147
12
XDOT = 16011
251143 XDOT = 4880
229348
YDOT = -6004
710994 feet/sec YDOT = -1830
235911 meter/sec
ZDOT = -17063
960527 ZDOT = -5201
095169
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 12170
53839852
00016717 00000-0 10270-3 0 9102
2 25544 51
6364 115
6321 0010526 76
9108 283
3220 15
56466607 18220
Satellite: ISS
Catalog Number: 25544
Epoch time: 12170
53839852 = yrday
fracday
Element set: 910
Inclination: 51
6364 deg
RA of node: 115
6321 deg
Eccentricity:
0010526
Arg of perigee: 76
9108 deg
Mean anomaly: 283
3220 deg
Mean motion: 15
56466607 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1822
Checksum: 296
Coasting Arc #12 (Orbit 1837)
---------------------------------------
Vector Time (GMT): 2012/171/12:16:42
072
Vector Time (MET): N/A
Weight (LBS) : 923792
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4540831
47 A = 6774002
66 meter
Y = 2270810
14 meter E =
0018932
Z = 4469310
96 I = 51
95591
XDOT = -223
308048 Wp = 95
19525
YDOT = -6940
531732 meter/sec RA = 109
89069 deg
ZDOT = 3285
950642 TA = 321
84146
MA = 321
97535
Ha = 221
188 n
mi
Hp = 207
162
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14897741
04 X = -4587597
52
Y = 7450164
50 feet Y = 2219769
50 meter
Z = 14663093
70 Z = 4447138
62
XDOT = -732
637954 XDOT = -161
643395
YDOT = -22770
773398 feet/sec YDOT = -6942
684680 meter/sec
ZDOT = 10780
677959 ZDOT = 3285
014410
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7840714
43 X = 2389849
76
Y = 14786788
42 feet Y = 4507013
11 meter
Z = 14571480
41 Z = 4441387
23
XDOT = -21663
115121 XDOT = -6602
917489
YDOT = 822
154046 feet/sec YDOT = 250
592553 meter/sec
ZDOT = 10777
492127 ZDOT = 3284
979600
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 12171
56567876
00016717 00000-0 10270-3 0 9111
2 25544 51
6369 110
4930 0010409 81
3360 278
8973 15
56508559 18388
Satellite: ISS
Catalog Number: 25544
Epoch time: 12171
56567876 = yrday
fracday
Element set: 911
Inclination: 51
6369 deg
RA of node: 110
4930 deg
Eccentricity:
0010409
Arg of perigee: 81
3360 deg
Mean anomaly: 278
8973 deg
Mean motion: 15
56508559 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1838
Checksum: 333
Coasting Arc #13 (Orbit 1852)
---------------------------------------
Vector Time (GMT): 2012/172/12:16:42
072
Vector Time (MET): N/A
Weight (LBS) : 923792
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4197183
65 A = 6770564
62 meter
Y = 411683
17 meter E =
0025137
Z = -5318406
42 I = 51
95437
XDOT = -1499
616711 Wp = 84
92199
YDOT = 7480
833407 meter/sec RA = 104
89125 deg
ZDOT = -604
689197 TA = 179
32188
MA = 179
31846
Ha = 221
073 n
mi
Hp = 207
237
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13770287
56 X = 4218103
68
Y = 1350666
58 feet Y = 458736
54 meter
Z = -17448839
97 Z = -5297965
90
XDOT = -4920
002332 XDOT = -1580
220034
YDOT = 24543
416690 feet/sec YDOT = 7463
613188 meter/sec
ZDOT = -1983
888442 ZDOT = -612
168761
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 746612
64 X = 227567
53
Y = -13921916
70 feet Y = -4243400
21 meter
Z = -17364617
50 Z = -5292735
41
XDOT = 23717
795413 XDOT = 7229
184042
YDOT = 3784
605756 feet/sec YDOT = 1153
547834 meter/sec
ZDOT = -2015
456888 ZDOT = -614
311260
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 12172
52873998
00016717 00000-0 10270-3 0 9124
2 25544 51
6374 105
6738 0010444 84
2623 275
9722 15
56510455 18534
Satellite: ISS
Catalog Number: 25544
Epoch time: 12172
52873998 = yrday
fracday
Element set: 912
Inclination: 51
6374 deg
RA of node: 105
6738 deg
Eccentricity:
0010444
Arg of perigee: 84
2623 deg
Mean anomaly: 275
9722 deg
Mean motion: 15
56510455 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1853
Checksum: 322
Coasting Arc #14 (Orbit 1853)
---------------------------------------
Vector Time (GMT): 2012/172/13:54:15
860
Vector Time (MET): N/A
Weight (LBS) : 923384
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3512738
17 A = 6773467
14 meter
Y = 2616263
17 meter E =
0020624
Z = -5184881
29 I = 51
95806
XDOT = -2975
833922 Wp = 95
47547
YDOT = 6899
033692 meter/sec RA = 104
53746 deg
ZDOT = 1468
195884 TA = 188
60081
MA = 188
63621
Ha = 221
091 n
mi
Hp = 209
723
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11524731
52 X = 3508408
36
Y = 8583540
60 feet Y = 2655521
45 meter
Z = -17010765
39 Z = -5167826
72
XDOT = -9763
234652 XDOT = -3059
891285
YDOT = 22634
624975 feet/sec YDOT = 6865
285838 meter/sec
ZDOT = 4816
915631 ZDOT = 1453
536466
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2382175
44 X = 726087
07
Y = -14254826
53 feet Y = -4344871
13 meter
Z = -16940717
39 Z = -5163530
66
XDOT = 23575
609413 XDOT = 7185
845749
YDOT = -1699
961952 feet/sec YDOT = -518
148403 meter/sec
ZDOT = 4755
805556 ZDOT = 1449
569533
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 12172
59294522
00016717 00000-0 10270-3 0 9132
2 25544 51
6386 105
3534 0007031 84
2355 275
9600 15
55706009 18545
Satellite: ISS
Catalog Number: 25544
Epoch time: 12172
59294522 = yrday
fracday
Element set: 913
Inclination: 51
6386 deg
RA of node: 105
3534 deg
Eccentricity:
0007031
Arg of perigee: 84
2355 deg
Mean anomaly: 275
9600 deg
Mean motion: 15
55706009 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1854
Checksum: 301
Coasting Arc #15 (Orbit 1869)
---------------------------------------
Vector Time (GMT): 2012/173/13:54:15
860
Vector Time (MET): N/A
Weight (LBS) : 923384
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2518450
86 A = 6777301
00 meter
Y = -4697721
53 meter E =
0017263
Z = 4173078
28 I = 51
97770
XDOT = 3896
930629 Wp = 80
42939
YDOT = -5443
193979 meter/sec RA = 99
55060 deg
ZDOT = -3759
742042 TA = 48
07769
MA = 47
93063
Ha = 221
116 n
mi
Hp = 209
582
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8262634
05 X = -2486004
51
Y = -15412472
20 feet Y = -4725703
64 meter
Z = 13691201
71 Z = 4160921
93
XDOT = 12785
205476 XDOT = 3975
771745
YDOT = -17858
247961 feet/sec YDOT = -5399
174675 meter/sec
ZDOT = -12335
111685 ZDOT = -3740
620416
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9707716
30 X = -2958911
93
Y = 14592215
47 feet Y = 4447707
27 meter
Z = 13641551
12 Z = 4157944
78
XDOT = -20738
279750 XDOT = -6321
027668
YDOT = -2290
008349 feet/sec YDOT = -697
994545 meter/sec
ZDOT = -12255
737309 ZDOT = -3735
548732
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 12173
62072740
00016717 00000-0 10270-3 0 9144
2 25544 51
6384 100
2172 0007030 87
6774 272
5185 15
55735771 18703
Satellite: ISS
Catalog Number: 25544
Epoch time: 12173
62072740 = yrday
fracday
Element set: 914
Inclination: 51
6384 deg
RA of node: 100
2172 deg
Eccentricity:
0007030
Arg of perigee: 87
6774 deg
Mean anomaly: 272
5185 deg
Mean motion: 15
55735771 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1870
Checksum: 301
Coasting Arc #16 (Orbit 1884)
---------------------------------------
Vector Time (GMT): 2012/174/13:54:15
860
Vector Time (MET): N/A
Weight (LBS) : 923384
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1436070
02 A = 6782016
60 meter
Y = 6155788
80 meter E =
0011517
Z = -2461277
44 I = 51
99859
XDOT = -4459
354868 Wp = 72
52219
YDOT = 3175
674605 meter/sec RA = 94
58027 deg
ZDOT = 5364
625583 TA = 260
06099
MA = 260
19101
Ha = 220
981 n
mi
Hp = 209
585
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4711515
83 X = 1379084
22
Y = 20196157
49 feet Y = 6171529
54 meter
Z = -8075057
20 Z = -2454438
70
XDOT = -14630
429357 XDOT = -4520
594373
YDOT = 10418
879937 feet/sec YDOT = 3125
464180 meter/sec
ZDOT = 17600
477634 ZDOT = 5342
814132
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15376454
11 X = 4686743
21
Y = -13931707
14 feet Y = -4246384
34 meter
Z = -8047478
03 Z = -2452871
30
XDOT = 15230
714530 XDOT = 4642
321789
YDOT = 6741
185103 feet/sec YDOT = 2054
713220 meter/sec
ZDOT = 17510
229785 ZDOT = 5337
118038
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 12174
58425770
00016717 00000-0 10270-3 0 9156
2 25544 51
6392 95
4015 0006941 91
4328 268
7620 15
55764245 18856
Satellite: ISS
Catalog Number: 25544
Epoch time: 12174
58425770 = yrday
fracday
Element set: 915
Inclination: 51
6392 deg
RA of node: 95
4015 deg
Eccentricity:
0006941
Arg of perigee: 91
4328 deg
Mean anomaly: 268
7620 deg
Mean motion: 15
55764245 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1885
Checksum: 326
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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