[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
August 6th 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) : 131 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 202 ET - UTC (sec) : 67 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
228/16:14:35
069 -5
0 9
3 9
3
N/A -5
2 0
2 224
6
000/00:29:10
138 5
8 -0
0 217
3
Coasting Arc #1 (Orbit 2538)
---------------------------------------
Vector Time (GMT): 2012/216/13:20:15
487
Vector Time (MET): N/A
Weight (LBS) : 954738
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4436732
07 A = 6775776
58 meter
Y = -193317
42 meter E =
0005768
Z = 5114988
15 I = 51
30291
XDOT = 2062
943629 Wp = 44
12257
YDOT = 7233
404511 meter/sec RA = 244
82226 deg
ZDOT = -1510
912173 TA = 60
52182
MA = 60
46429
Ha = 219
739 n
mi
Hp = 213
338
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14556207
59 X = 4413717
16
Y = -634243
50 feet Y = -143831
91 meter
Z = 16781457
19 Z = 5136485
19
XDOT = 6768
187760 XDOT = 1989
244387
YDOT = 23731
642097 feet/sec YDOT = 7256
061585 meter/sec
ZDOT = -4957
060935 ZDOT = -1501
069578
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13035314
45 X = -3973163
85
Y = -6275422
02 feet Y = -1912748
63 meter
Z = 16870163
17 Z = 5142025
73
XDOT = 4771
677464 XDOT = 1454
407291
YDOT = -23175
124093 feet/sec YDOT = -7063
777824 meter/sec
ZDOT = -4917
117069 ZDOT = -1498
737283
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 12216
60138474
00016717 00000-0 10270-3 0 9002
2 25544 51
6392 245
5244 0001457 6
3306 353
7865 15
54924179 25392
Satellite: ISS
Catalog Number: 25544
Epoch time: 12216
60138474 = yrday
fracday
Element set: 900
Inclination: 51
6392 deg
RA of node: 245
5244 deg
Eccentricity:
0001457
Arg of perigee: 6
3306 deg
Mean anomaly: 353
7865 deg
Mean motion: 15
54924179 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2539
Checksum: 308
Coasting Arc #2 (Orbit 2553)
---------------------------------------
Vector Time (GMT): 2012/217/13:20:15
487
Vector Time (MET): N/A
Weight (LBS) : 954738
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4970290
39 A = 6779155
96 meter
Y = -1723692
77 meter E =
0008298
Z = -4283766
45 I = 51
32835
XDOT = -681
742478 Wp = 100
09603
YDOT = -6771
570853 meter/sec RA = 239
79742 deg
ZDOT = 3520
135906 TA = 205
92896
MA = 205
97056
Ha = 219
878 n
mi
Hp = 213
222
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16306727
00 X = -4929837
14
Y = -5655160
02 feet Y = -1779047
45 meter
Z = -14054351
86 Z = -4307813
16
XDOT = -2236
687921 XDOT = -623
070394
YDOT = -22216
439807 feet/sec YDOT = -6778
866479 meter/sec
ZDOT = 11549
002315 ZDOT = 3516
966585
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11834956
13 X = 3607294
63
Y = 12451096
79 feet Y = 3795094
30 meter
Z = -14153409
08 Z = -4313959
09
XDOT = -7205
494277 XDOT = -2196
234656
YDOT = 19946
422672 feet/sec YDOT = 6079
669630 meter/sec
ZDOT = 11536
534450 ZDOT = 3516
335700
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 12217
56541997
00016717 00000-0 10270-3 0 9017
2 25544 51
6395 240
7127 0001559 6
8754 353
2420 15
54914559 25547
Satellite: ISS
Catalog Number: 25544
Epoch time: 12217
56541997 = yrday
fracday
Element set: 901
Inclination: 51
6395 deg
RA of node: 240
7127 deg
Eccentricity:
0001559
Arg of perigee: 6
8754 deg
Mean anomaly: 353
2420 deg
Mean motion: 15
54914559 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2554
Checksum: 318
Coasting Arc #3 (Orbit 2569)
---------------------------------------
Vector Time (GMT): 2012/218/13:20:15
487
Vector Time (MET): N/A
Weight (LBS) : 954738
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5150923
53 A = 6783399
52 meter
Y = 3380724
35 meter E =
0013464
Z = 2825376
29 I = 51
35848
XDOT = -942
588354 Wp = 92
34723
YDOT = 5685
140719 meter/sec RA = 234
78531 deg
ZDOT = -5063
789086 TA = 55
39902
MA = 55
27210
Ha = 219
804 n
mi
Hp = 213
172
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16899355
40 X = 5099011
92
Y = 11091615
33 feet Y = 3438034
94 meter
Z = 9269607
26 Z = 2850272
73
XDOT = -3092
481477 XDOT = -981
492365
YDOT = 18652
036481 feet/sec YDOT = 5674
382554 meter/sec
ZDOT = -16613
481253 ZDOT = -5068
462595
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10201297
85 X = -3109355
58
Y = -17396445
42 feet Y = -5302436
56 meter
Z = 9372031
32 Z = 2856595
15
XDOT = 9661
385234 XDOT = 2944
790219
YDOT = -14661
959880 feet/sec YDOT = -4468
965371 meter/sec
ZDOT = -16633
266295 ZDOT = -5069
819567
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 12218
59371174
00016717 00000-0 10270-3 0 9020
2 25544 51
6386 235
5787 0001665 9
9055 350
2131 15
54977852 25706
Satellite: ISS
Catalog Number: 25544
Epoch time: 12218
59371174 = yrday
fracday
Element set: 902
Inclination: 51
6386 deg
RA of node: 235
5787 deg
Eccentricity:
0001665
Arg of perigee: 9
9055 deg
Mean anomaly: 350
2131 deg
Mean motion: 15
54977852 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2570
Checksum: 320
Coasting Arc #4 (Orbit 2584)
---------------------------------------
Vector Time (GMT): 2012/219/13:20:15
487
Vector Time (MET): N/A
Weight (LBS) : 954738
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4907874
54 A = 6786327
52 meter
Y = -4572044
78 meter E =
0011102
Z = -996892
08 I = 51
38689
XDOT = 2662
792864 Wp = 36
27490
YDOT = -4132
707967 meter/sec RA = 229
78820 deg
ZDOT = 5886
849016 TA = 312
88085
MA = 312
97402
Ha = 219
826 n
mi
Hp = 213
073
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16101950
58 X = -4851541
61
Y = -15000146
90 feet Y = -4626612
71 meter
Z = -3270643
31 Z = -1020597
16
XDOT = 8736
197060 XDOT = 2680
211125
YDOT = -13558
753171 feet/sec YDOT = -4102
833531 meter/sec
ZDOT = 19313
809109 ZDOT = 5899
826918
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8143425
43 X = 2482116
07
Y = 20428292
70 feet Y = 6226543
62 meter
Z = -3368056
81 Z = -1026583
72
XDOT = -12089
394226 XDOT = -3684
847360
YDOT = 7990
171098 feet/sec YDOT = 2435
404151 meter/sec
ZDOT = 19367
719055 ZDOT = 5903
280768
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 12219
55772498
00016717 00000-0 10270-3 0 9032
2 25544 51
6386 230
7670 0001498 19
4817 340
6393 15
55006685 25857
Satellite: ISS
Catalog Number: 25544
Epoch time: 12219
55772498 = yrday
fracday
Element set: 903
Inclination: 51
6386 deg
RA of node: 230
7670 deg
Eccentricity:
0001498
Arg of perigee: 19
4817 deg
Mean anomaly: 340
6393 deg
Mean motion: 15
55006685 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2585
Checksum: 333
Coasting Arc #5 (Orbit 2600)
---------------------------------------
Vector Time (GMT): 2012/220/13:20:15
487
Vector Time (MET): N/A
Weight (LBS) : 954738
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4154042
67 A = 6786401
64 meter
Y = 5265640
65 meter E =
0008946
Z = -1014549
96 I = 51
40725
XDOT = -4345
233452 Wp = 132
36712
YDOT = 2301
980439 meter/sec RA = 224
79630 deg
ZDOT = -5883
006986 TA = 58
66506
MA = 58
57753
Ha = 219
934 n
mi
Hp = 213
089
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13628748
91 X = 4099780
86
Y = 17275723
91 feet Y = 5311790
34 meter
Z = -3328575
99 Z = -994501
80
XDOT = -14256
015261 XDOT = -4342
073681
YDOT = 7552
429261 feet/sec YDOT = 2253
407008 meter/sec
ZDOT = -19301
204021 ZDOT = -5904
108052
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5340589
52 X = -1627811
69
Y = -21359130
92 feet Y = -6510263
10 meter
Z = -3246302
74 Z = -989473
08
XDOT = 14434
583121 XDOT = 4399
660935
YDOT = -682
418965 feet/sec YDOT = -208
001300 meter/sec
ZDOT = -19388
475707 ZDOT = -5909
607395
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 12220
58599328
00016717 00000-0 10270-3 0 9047
2 25544 51
6385 225
6329 0001727 18
0946 342
0269 15
54991875 26013
Satellite: ISS
Catalog Number: 25544
Epoch time: 12220
58599328 = yrday
fracday
Element set: 904
Inclination: 51
6385 deg
RA of node: 225
6329 deg
Eccentricity:
0001727
Arg of perigee: 18
0946 deg
Mean anomaly: 342
0269 deg
Mean motion: 15
54991875 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2601
Checksum: 324
Coasting Arc #6 (Orbit 2616)
---------------------------------------
Vector Time (GMT): 2012/221/13:20:15
487
Vector Time (MET): N/A
Weight (LBS) : 954738
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2928880
41 A = 6783252
18 meter
Y = -5403361
22 meter E =
0014119
Z = 2853460
36 I = 51
41940
XDOT = 5759
733425 Wp = 75
22829
YDOT = -445
520045 meter/sec RA = 219
80204 deg
ZDOT = 5050
916657 TA = 317
36529
MA = 317
47479
Ha = 219
810 n
mi
Hp = 213
057
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9609187
68 X = -2882102
58
Y = -17727563
07 feet Y = -5435852
27 meter
Z = 9361746
59 Z = 2839345
66
XDOT = 18896
763206 XDOT = 5739
751231
YDOT = -1461
679937 feet/sec YDOT = -381
222916 meter/sec
ZDOT = 16571
248876 ZDOT = 5078
848414
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1870570
32 X = 570149
83
Y = 20104291
56 feet Y = 6127788
07 meter
Z = 9303961
91 Z = 2835847
59
XDOT = -16375
360134 XDOT = -4991
209769
YDOT = -6225
262848 feet/sec YDOT = -1897
460116 meter/sec
ZDOT = 16686
555160 ZDOT = 5086
062013
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 12221
61424686
00016717 00000-0 10270-3 0 9057
2 25544 51
6384 220
5003 0001539 17
0144 343
1060 15
55045561 26176
Satellite: ISS
Catalog Number: 25544
Epoch time: 12221
61424686 = yrday
fracday
Element set: 905
Inclination: 51
6384 deg
RA of node: 220
5003 deg
Eccentricity:
0001539
Arg of perigee: 17
0144 deg
Mean anomaly: 343
1060 deg
Mean motion: 15
55045561 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2617
Checksum: 267
Coasting Arc #7 (Orbit 2631)
---------------------------------------
Vector Time (GMT): 2012/222/13:20:15
487
Vector Time (MET): N/A
Weight (LBS) : 954738
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1266962
13 A = 6778852
64 meter
Y = 5076274
60 meter E =
0009815
Z = -4320702
56 I = 51
42858
XDOT = -6704
955980 Wp = 62
46243
YDOT = -1283
710097 meter/sec RA = 214
79508 deg
ZDOT = -3475
924453 TA = 172
07032
MA = 172
05479
Ha = 219
933 n
mi
Hp = 212
997
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4156699
91 X = 1231092
85
Y = 16654444
24 feet Y = 5090242
12 meter
Z = -14175533
32 Z = -4314634
76
XDOT = -21997
887072 XDOT = -6673
217815
YDOT = -4211
647299 feet/sec YDOT = -1358
511537 meter/sec
ZDOT = -11403
951616 ZDOT = -3508
419516
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2393848
48 X = 729645
02
Y = -17018086
20 feet Y = -5187112
67 meter
Z = -14150923
78 Z = -4313201
57
XDOT = 17448
027810 XDOT = 5318
158877
YDOT = 12043
939694 feet/sec YDOT = 3670
992819 meter/sec
ZDOT = -11537
953813 ZDOT = -3516
768322
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 12222
57822604
00016717 00000-0 10270-3 0 9066
2 25544 51
6384 215
6870 0001767 23
2092 336
9141 15
55021498 26327
Satellite: ISS
Catalog Number: 25544
Epoch time: 12222
57822604 = yrday
fracday
Element set: 906
Inclination: 51
6384 deg
RA of node: 215
6870 deg
Eccentricity:
0001767
Arg of perigee: 23
2092 deg
Mean anomaly: 336
9141 deg
Mean motion: 15
55021498 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2632
Checksum: 297
Coasting Arc #8 (Orbit 2647)
---------------------------------------
Vector Time (GMT): 2012/223/13:20:15
487
Vector Time (MET): N/A
Weight (LBS) : 954738
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 651500
50 A = 6775352
06 meter
Y = -4353649
86 meter E =
0004508
Z = 5146812
18 I = 51
44288
XDOT = 7032
141244 Wp = 102
98258
YDOT = 2725
714755 meter/sec RA = 209
77786 deg
ZDOT = 1413
471243 TA = 333
38097
MA = 333
40411
Ha = 219
827 n
mi
Hp = 212
955
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2137468
85 X = 675133
66
Y = -14283628
14 feet Y = -4346232
42 meter
Z = 16885866
74 Z = 5150034
36
XDOT = 23071
329540 XDOT = 6994
272828
YDOT = 8942
633711 feet/sec YDOT = 2804
140745 meter/sec
ZDOT = 4637
372845 ZDOT = 1447
540894
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7086907
46 X = -2160089
39
Y = 12566014
54 feet Y = 3830121
23 meter
Z = 16899536
17 Z = 5150978
63
XDOT = -17299
000177 XDOT = -5272
735254
YDOT = -16190
606098 feet/sec YDOT = -4934
896739 meter/sec
ZDOT = 4777
766133 ZDOT = 1456
263117
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 12223
60645531
00016717 00000-0 10270-3 0 9074
2 25544 51
6384 210
5543 0001779 21
1276 338
9950 15
55054836 26481
Satellite: ISS
Catalog Number: 25544
Epoch time: 12223
60645531 = yrday
fracday
Element set: 907
Inclination: 51
6384 deg
RA of node: 210
5543 deg
Eccentricity:
0001779
Arg of perigee: 21
1276 deg
Mean anomaly: 338
9950 deg
Mean motion: 15
55054836 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2648
Checksum: 309
Coasting Arc #9 (Orbit 2662)
---------------------------------------
Vector Time (GMT): 2012/224/13:20:15
487
Vector Time (MET): N/A
Weight (LBS) : 954738
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2640501
21 A = 6774884
25 meter
Y = 3388189
42 meter E =
0015239
Z = -5252201
77 I = 51
46847
XDOT = -6593
345510 Wp = 90
32625
YDOT = -3799
459156 meter/sec RA = 204
75457 deg
ZDOT = 865
817343 TA = 187
97075
MA = 187
99500
Ha = 219
912 n
mi
Hp = 212
791
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8663061
71 X = -2652678
65
Y = 11116107
03 feet Y = 3358593
83 meter
Z = -17231633
10 Z = -5265058
50
XDOT = -21631
710991 XDOT = -6554
575043
YDOT = -12465
417180 feet/sec YDOT = -3872
973304 meter/sec
ZDOT = 2840
608081 ZDOT = 833
881505
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11886170
96 X = 3622904
91
Y = -7449404
72 feet Y = -2270578
56 meter
Z = -17284992
39 Z = -5268465
68
XDOT = 15425
997287 XDOT = 4701
843973
YDOT = 18343
439897 feet/sec YDOT = 5591
080481 meter/sec
ZDOT = 2709
096575 ZDOT = 825
732636
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 12224
57040854
00016717 00000-0 10270-3 0 9089
2 25544 51
6385 205
7413 0001818 26
1438 333
9807 15
55055909 26638
Satellite: ISS
Catalog Number: 25544
Epoch time: 12224
57040854 = yrday
fracday
Element set: 908
Inclination: 51
6385 deg
RA of node: 205
7413 deg
Eccentricity:
0001818
Arg of perigee: 26
1438 deg
Mean anomaly: 333
9807 deg
Mean motion: 15
55055909 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2663
Checksum: 311
Coasting Arc #10 (Orbit 2678)
---------------------------------------
Vector Time (GMT): 2012/225/13:20:15
487
Vector Time (MET): N/A
Weight (LBS) : 954738
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4457037
58 A = 6777542
18 meter
Y = -2263574
23 meter E =
0009963
Z = 4571824
35 I = 51
50613
XDOT = 5414
823439 Wp = 59
50814
YDOT = 4508
547107 meter/sec RA = 199
73773 deg
ZDOT = -3036
732178 TA = 60
91868
MA = 60
81894
Ha = 219
772 n
mi
Hp = 212
810
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14622826
70 X = 4459809
47
Y = -7426424
64 feet Y = -2213717
58 meter
Z = 14999423
71 Z = 4593482
79
XDOT = 17765
168763 XDOT = 5378
757062
YDOT = 14791
821216 feet/sec YDOT = 4568
897510 meter/sec
ZDOT = -9963
032080 ZDOT = -3010
514942
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16170159
95 X = -4928664
75
Y = 2192853
61 feet Y = 668381
78 meter
Z = 15089031
64 Z = 4599136
84
XDOT = -11759
829038 XDOT = -3584
395891
YDOT = -18681
788202 feet/sec YDOT = -5694
209044 meter/sec
ZDOT = -9855
171256 ZDOT = -3003
856199
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 12225
59861162
00016717 00000-0 10270-3 0 9096
2 25544 51
6387 200
6080 0001838 27
5096 332
6155 15
55090860 26795
Satellite: ISS
Catalog Number: 25544
Epoch time: 12225
59861162 = yrday
fracday
Element set: 909
Inclination: 51
6387 deg
RA of node: 200
6080 deg
Eccentricity:
0001838
Arg of perigee: 27
5096 deg
Mean anomaly: 332
6155 deg
Mean motion: 15
55090860 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2679
Checksum: 315
Coasting Arc #11 (Orbit 2693)
---------------------------------------
Vector Time (GMT): 2012/226/13:20:15
487
Vector Time (MET): N/A
Weight (LBS) : 954738
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5849361
81 A = 6781962
25 meter
Y = 1125670
59 meter E =
0005946
Z = -3244812
29 I = 51
54995
XDOT = -3564
363870 Wp = 69
34863
YDOT = -4841
339208 meter/sec RA = 194
73496 deg
ZDOT = 4754
997104 TA = 253
00252
MA = 253
06769
Ha = 219
859 n
mi
Hp = 212
711
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19190819
57 X = -5845752
23
Y = 3693144
97 feet Y = 1060279
71 meter
Z = -10645709
62 Z = -3273218
97
XDOT = -11694
107185 XDOT = -3533
060441
YDOT = -15883
658820 feet/sec YDOT = -4881
023319 meter/sec
ZDOT = 15600
384200 ZDOT = 4737
757683
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19314917
46 X = 5887186
84
Y = 2519468
22 feet Y = 767933
91 meter
Z = -10763096
79 Z = -3280591
90
XDOT = 6370
323129 XDOT = 1941
674490
YDOT = 17379
085992 feet/sec YDOT = 5297
145410 meter/sec
ZDOT = 15529
604305 ZDOT = 4733
423392
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 12226
56253927
00016717 00000-0 10270-3 0 9100
2 25544 51
6386 195
7953 0001881 29
5391 330
5868 15
55091214 26944
Satellite: ISS
Catalog Number: 25544
Epoch time: 12226
56253927 = yrday
fracday
Element set: 910
Inclination: 51
6386 deg
RA of node: 195
7953 deg
Eccentricity:
0001881
Arg of perigee: 29
5391 deg
Mean anomaly: 330
5868 deg
Mean motion: 15
55091214 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2694
Checksum: 328
Coasting Arc #12 (Orbit 2709)
---------------------------------------
Vector Time (GMT): 2012/227/13:20:15
487
Vector Time (MET): N/A
Weight (LBS) : 954738
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6633539
63 A = 6785558
72 meter
Y = 13171
57 meter E =
0014171
Z = 1400340
60 I = 51
59286
XDOT = 1222
859989 Wp = 111
83441
YDOT = 4872
992033 meter/sec RA = 189
74803 deg
ZDOT = -5796
702362 TA = 52
88284
MA = 52
75343
Ha = 219
876 n
mi
Hp = 212
657
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21763581
48 X = 6626096
92
Y = 43213
81 feet Y = 87310
28 meter
Z = 4594293
32 Z = 1432547
36
XDOT = 4012
007838 XDOT = 1196
436847
YDOT = 15987
506671 feet/sec YDOT = 4886
519262 meter/sec
ZDOT = -19018
052368 ZDOT = -5790
825896
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20730489
26 X = -6318653
12
Y = -6531645
13 feet Y = -1990845
44 meter
Z = 4727293
56 Z = 1440879
08
XDOT = 357
330710 XDOT = 108
914400
YDOT = -14977
967204 feet/sec YDOT = -4565
284404 meter/sec
ZDOT = -18994
186685 ZDOT = -5789
428102
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 12227
59071549
00016717 00000-0 10270-3 0 9113
2 25544 51
6395 190
6613 0001868 34
5957 325
5318 15
55123863 27109
Satellite: ISS
Catalog Number: 25544
Epoch time: 12227
59071549 = yrday
fracday
Element set: 911
Inclination: 51
6395 deg
RA of node: 190
6613 deg
Eccentricity:
0001868
Arg of perigee: 34
5957 deg
Mean anomaly: 325
5318 deg
Mean motion: 15
55123863 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2710
Checksum: 316
Coasting Arc #13 (Orbit 2725)
---------------------------------------
Vector Time (GMT): 2012/228/13:20:15
487
Vector Time (MET): N/A
Weight (LBS) : 954738
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6667915
36 A = 6786219
04 meter
Y = -1050921
00 meter E =
0014870
Z = 622226
31 I = 51
62543
XDOT = 1296
247676 Wp = 49
80515
YDOT = -4637
914507 meter/sec RA = 184
77070 deg
ZDOT = 5972
780988 TA = 316
91864
MA = 317
03493
Ha = 219
849 n
mi
Hp = 212
667
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21876362
73 X = -6658690
74
Y = -3447903
55 feet Y = -1125434
21 meter
Z = 2041424
90 Z = 589856
94
XDOT = 4252
781089 XDOT = 1318
999632
YDOT = -15216
254944 feet/sec YDOT = -4623
291930 meter/sec
ZDOT = 19595
738148 ZDOT = 5979
133168
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20026423
44 X = 6104053
87
Y = 9483315
98 feet Y = 2890514
71 meter
Z = 1907821
44 Z = 581503
97
XDOT = -7566
186344 XDOT = -2306
173598
YDOT = 11970
468342 feet/sec YDOT = 3648
598751 meter/sec
ZDOT = 19622
351719 ZDOT = 5980
892804
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 12228
61887669
00016717 00000-0 10270-3 0 9126
2 25544 51
6395 185
5276 0001847 36
2021 323
9257 15
55151078 27265
Satellite: ISS
Catalog Number: 25544
Epoch time: 12228
61887669 = yrday
fracday
Element set: 912
Inclination: 51
6395 deg
RA of node: 185
5276 deg
Eccentricity:
0001847
Arg of perigee: 36
2021 deg
Mean anomaly: 323
9257 deg
Mean motion: 15
55151078 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2726
Checksum: 325
Coasting Arc #14 (Orbit 2727)
---------------------------------------
Vector Time (GMT): 2012/228/16:29:10
138
Vector Time (MET): N/A
Weight (LBS) : 953457
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6172864
75 A = 6791944
76 meter
Y = -2004558
10 meter E =
0016706
Z = 1963807
46 I = 51
62642
XDOT = 3148
044283 Wp = 32
12691
YDOT = -4210
352925 meter/sec RA = 184
12786 deg
ZDOT = 5589
559236 TA = 349
55261
MA = 349
58728
Ha = 224
633 n
mi
Hp = 217
302
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20252180
92 X = -6159530
12
Y = -6576634
17 feet Y = -2073512
37 meter
Z = 6442937
86 Z = 1933852
95
XDOT = 10328
229274 XDOT = 3167
739098
YDOT = -13813
493847 feet/sec YDOT = -4175
039478 meter/sec
ZDOT = 18338
448937 ZDOT = 5604
899765
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20782564
45 X = 6334525
64
Y = -4802582
79 feet Y = -1463827
23 meter
Z = 6319383
74 Z = 1926148
17
XDOT = -2002
304462 XDOT = -610
302400
YDOT = 15584
659526 feet/sec YDOT = 4750
204224 meter/sec
ZDOT = 18402
151003 ZDOT = 5608
975626
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 12228
74749701
00016717 00000-0 10270-3 0 9135
2 25544 51
6414 184
8874 0009738 335
4302 24
6385 15
52690940 27288
Satellite: ISS
Catalog Number: 25544
Epoch time: 12228
74749701 = yrday
fracday
Element set: 913
Inclination: 51
6414 deg
RA of node: 184
8874 deg
Eccentricity:
0009738
Arg of perigee: 335
4302 deg
Mean anomaly: 24
6385 deg
Mean motion: 15
52690940 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2728
Checksum: 327
Coasting Arc #15 (Orbit 2742)
---------------------------------------
Vector Time (GMT): 2012/229/16:29:10
138
Vector Time (MET): N/A
Weight (LBS) : 953457
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5589447
75 A = 6789574
33 meter
Y = 2345696
95 meter E =
0007508
Z = -3068181
88 I = 51
64959
XDOT = -4354
324963 Wp = 4
65267
YDOT = 3947
502480 meter/sec RA = 179
15894 deg
ZDOT = -4908
049365 TA = 210
50693
MA = 210
55063
Ha = 224
640 n
mi
Hp = 217
236
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18338083
16 X = 5577706
48
Y = 7695856
12 feet Y = 2408135
94 meter
Z = -10066213
51 Z = -3041057
72
XDOT = -14285
843055 XDOT = -4374
301439
YDOT = 12951
123622 feet/sec YDOT = 3898
697955 meter/sec
ZDOT = -16102
524165 ZDOT = -4929
250599
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19683886
74 X = -5999648
68
Y = 3208647
28 feet Y = 977995
69 meter
Z = -9954362
62 Z = -3034089
73
XDOT = 5417
455517 XDOT = 1651
240442
YDOT = -17060
848723 feet/sec YDOT = -5200
146691 meter/sec
ZDOT = -16190
416715 ZDOT = -4934
839015
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 12229
71290630
00016717 00000-0 10270-3 0 9146
2 25544 51
6419 180
0848 0009699 337
5539 22
5187 15
52706606 27434
Satellite: ISS
Catalog Number: 25544
Epoch time: 12229
71290630 = yrday
fracday
Element set: 914
Inclination: 51
6419 deg
RA of node: 180
0848 deg
Eccentricity:
0009699
Arg of perigee: 337
5539 deg
Mean anomaly: 22
5187 deg
Mean motion: 15
52706606 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2743
Checksum: 324
Coasting Arc #16 (Orbit 2758)
---------------------------------------
Vector Time (GMT): 2012/230/16:29:10
138
Vector Time (MET): N/A
Weight (LBS) : 953457
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4766641
10 A = 6786719
53 meter
Y = -2692408
41 meter E =
0010714
Z = 3998877
07 I = 51
67093
XDOT = 5421
111095 Wp = 47
35794
YDOT = -3705
009010 meter/sec RA = 174
18597 deg
ZDOT = 3967
727030 TA = 1
39905
MA = 1
39605
Ha = 224
907 n
mi
Hp = 216
818
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15638586
28 X = -4755605
02
Y = -8833360
92 feet Y = -2745650
11 meter
Z = 13119675
42 Z = 3975748
30
XDOT = 17785
797557 XDOT = 5442
864423
YDOT = -12155
541370 feet/sec YDOT = -3644
265005 meter/sec
ZDOT = 13017
477134 ZDOT = 3994
114984
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17994407
54 X = 5484695
42
Y = -1134579
05 feet Y = -345819
70 meter
Z = 13024344
77 Z = 3969820
29
XDOT = -8332
859458 XDOT = -2539
855563
YDOT = 18516
329840 feet/sec YDOT = 5643
777335 meter/sec
ZDOT = 13126
782293 ZDOT = 4001
043243
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 12230
74266498
00016717 00000-0 10270-3 0 9157
2 25544 51
6422 174
9612 0009778 342
6262 17
4554 15
52727662 27590
Satellite: ISS
Catalog Number: 25544
Epoch time: 12230
74266498 = yrday
fracday
Element set: 915
Inclination: 51
6422 deg
RA of node: 174
9612 deg
Eccentricity:
0009778
Arg of perigee: 342
6262 deg
Mean anomaly: 17
4554 deg
Mean motion: 15
52727662 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2759
Checksum: 331
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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