[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
May 28th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10763 91 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 130 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 186 ET - UTC (sec) : 66 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
There are no maneuvers
Coasting Arc #1 (Orbit 1494)
---------------------------------------
Vector Time (GMT): 2012/149/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 941021
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5679793
21 A = 6778443
18 meter
Y = 1049971
17 meter E =
0016127
Z = 3547065
34 I = 51
41312
XDOT = 1678
951474 Wp = 49
09089
YDOT = 6018
282000 meter/sec RA = 219
81412 deg
ZDOT = -4446
298007 TA = 88
88256
MA = 88
69780
Ha = 220
313 n
mi
Hp = 210
571
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18634492
14 X = 5650399
16
Y = 3444787
31 feet Y = 1113321
55 meter
Z = 11637353
49 Z = 3574586
32
XDOT = 5508
370978 XDOT = 1633
128244
YDOT = 19745
019686 feet/sec YDOT = 6036
801154 meter/sec
ZDOT = -14587
591887 ZDOT = -4438
252609
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10798456
04 X = 3291369
40
Y = -15487395
80 feet Y = -4720558
24 meter
Z = 11750437
10 Z = 3581533
23
XDOT = 19165
033143 XDOT = 5841
502102
YDOT = 2261
386493 feet/sec YDOT = 689
270603 meter/sec
ZDOT = -14555
003639 ZDOT = -4436
365109
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 12149
53972023
00016717 00000-0 10270-3 0 9005
2 25544 51
6382 220
6514 0009985
6847 359
4319 15
56002307 14955
Satellite: ISS
Catalog Number: 25544
Epoch time: 12149
53972023 = yrday
fracday
Element set: 900
Inclination: 51
6382 deg
RA of node: 220
6514 deg
Eccentricity:
0009985
Arg of perigee:
6847 deg
Mean anomaly: 359
4319 deg
Mean motion: 15
56002307 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1495
Checksum: 304
Coasting Arc #2 (Orbit 1509)
---------------------------------------
Vector Time (GMT): 2012/150/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 941021
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6023073
93 A = 6782945
78 meter
Y = -2682737
25 meter E =
0017372
Z = -1550829
59 I = 51
45117
XDOT = 773
169360 Wp = 19
31092
YDOT = -5035
517957 meter/sec RA = 214
81082 deg
ZDOT = 5742
449532 TA = 323
66610
MA = 323
78392
Ha = 220
493 n
mi
Hp = 210
475
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19760741
24 X = -5985093
72
Y = -8801631
40 feet Y = -2749878
54 meter
Z = -5088023
59 Z = -1579997
55
XDOT = 2536
644881 XDOT = 801
524339
YDOT = -16520
728204 feet/sec YDOT = -5026
713691 meter/sec
ZDOT = 18840
057519 ZDOT = 5746
274164
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15909743
23 X = -4849289
74
Y = 14615161
10 feet Y = 4454701
10 meter
Z = -5207756
70 Z = -1587324
24
XDOT = -13135
580765 XDOT = -4003
725017
YDOT = -7619
520054 feet/sec YDOT = -2322
429713 meter/sec
ZDOT = 18856
196583 ZDOT = 5747
368719
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 12150
50310054
00016717 00000-0 10270-3 0 9015
2 25544 51
6376 215
8351 0010112 4
1704 355
9532 15
55957593 15109
Satellite: ISS
Catalog Number: 25544
Epoch time: 12150
50310054 = yrday
fracday
Element set: 901
Inclination: 51
6376 deg
RA of node: 215
8351 deg
Eccentricity:
0010112
Arg of perigee: 4
1704 deg
Mean anomaly: 355
9532 deg
Mean motion: 15
55957593 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1510
Checksum: 268
Coasting Arc #3 (Orbit 1525)
---------------------------------------
Vector Time (GMT): 2012/151/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 941021
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5508772
45 A = 6783574
31 meter
Y = 3882598
87 meter E =
0008479
Z = -790409
75 I = 51
47950
XDOT = -3331
702773 Wp = 76
69186
YDOT = 3530
598953 meter/sec RA = 209
81952 deg
ZDOT = -5929
356884 TA = 111
87016
MA = 111
77997
Ha = 220
619 n
mi
Hp = 210
149
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18073400
43 X = 5468786
69
Y = 12738185
27 feet Y = 3943977
85 meter
Z = -2593207
85 Z = -763744
95
XDOT = -10930
783376 XDOT = -3342
131206
YDOT = 11583
329898 feet/sec YDOT = 3493
283837 meter/sec
ZDOT = -19453
270617 ZDOT = -5945
567461
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18669938
02 X = 5690597
11
Y = -11870036
37 feet Y = -3617987
08 meter
Z = -2483856
87 Z = -757079
57
XDOT = 5722
556107 XDOT = 1744
235102
YDOT = 13048
373394 feet/sec YDOT = 3977
144210 meter/sec
ZDOT = -19520
227178 ZDOT = -5949
765244
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 12151
53069391
00016717 00000-0 10270-3 0 9025
2 25544 51
6377 210
6970 0010120 9
0478 351
0857 15
56023318 15265
Satellite: ISS
Catalog Number: 25544
Epoch time: 12151
53069391 = yrday
fracday
Element set: 902
Inclination: 51
6377 deg
RA of node: 210
6970 deg
Eccentricity:
0010120
Arg of perigee: 9
0478 deg
Mean anomaly: 351
0857 deg
Mean motion: 15
56023318 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1526
Checksum: 284
Coasting Arc #4 (Orbit 1541)
---------------------------------------
Vector Time (GMT): 2012/152/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 941021
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4116855
83 A = 6780192
26 meter
Y = -4489610
70 meter E =
0019381
Z = 2949190
14 I = 51
49468
XDOT = 5552
918432 Wp = 53
02103
YDOT = -1806
133647 meter/sec RA = 204
82451 deg
ZDOT = 4990
754354 TA = 340
81775
MA = 340
89062
Ha = 220
777 n
mi
Hp = 209
950
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13506744
84 X = -4080672
84
Y = -14729693
91 feet Y = -4535445
84 meter
Z = 9675820
67 Z = 2929277
88
XDOT = 18218
236324 XDOT = 5548
457935
YDOT = -5925
635325 feet/sec YDOT = -1744
062780 meter/sec
ZDOT = 16373
865990 ZDOT = 5017
719646
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18665087
57 X = -5689118
69
Y = 7251328
32 feet Y = 2210204
87 meter
Z = 9594284
13 Z = 2924337
80
XDOT = 1628
176537 XDOT = 496
268208
YDOT = -17669
406191 feet/sec YDOT = -5385
635007 meter/sec
ZDOT = 16484
923431 ZDOT = 5024
604662
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 12152
55827461
00016717 00000-0 10270-3 0 9039
2 25544 51
6374 205
5590 0010167 13
1495 346
9922 15
56022019 15420
Satellite: ISS
Catalog Number: 25544
Epoch time: 12152
55827461 = yrday
fracday
Element set: 903
Inclination: 51
6374 deg
RA of node: 205
5590 deg
Eccentricity:
0010167
Arg of perigee: 13
1495 deg
Mean anomaly: 346
9922 deg
Mean motion: 15
56022019 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1542
Checksum: 293
Coasting Arc #5 (Orbit 1556)
---------------------------------------
Vector Time (GMT): 2012/153/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 941021
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2024610
41 A = 6774990
55 meter
Y = 4591722
10 meter E =
0017947
Z = -4569015
68 I = 51
50573
XDOT = -7021
611219 Wp = 43
18842
YDOT = 51
609727 meter/sec RA = 199
81387 deg
ZDOT = -3053
845248 TA = 196
14789
MA = 196
20516
Ha = 220
813 n
mi
Hp = 209
771
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6642422
60 X = 1995310
01
Y = 15064705
05 feet Y = 4614199
16 meter
Z = -14990208
91 Z = -4559250
76
XDOT = -23036
782213 XDOT = -7006
831299
YDOT = 169
323252 feet/sec YDOT = -26
827341 meter/sec
ZDOT = -10019
177322 ZDOT = -3087
920644
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16466666
33 X = 5019039
90
Y = -1052349
95 feet Y = -320756
26 meter
Z = -14950416
02 Z = -4556886
80
XDOT = -7937
876704 XDOT = -2419
464819
YDOT = 20388
488898 feet/sec YDOT = 6214
411416 meter/sec
ZDOT = -10159
350447 ZDOT = -3096
570016
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 12153
52162035
00016717 00000-0 10270-3 0 9047
2 25544 51
6376 200
7421 0010167 16
6452 343
5033 15
56038684 15570
Satellite: ISS
Catalog Number: 25544
Epoch time: 12153
52162035 = yrday
fracday
Element set: 904
Inclination: 51
6376 deg
RA of node: 200
7421 deg
Eccentricity:
0010167
Arg of perigee: 16
6452 deg
Mean anomaly: 343
5033 deg
Mean motion: 15
56038684 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1557
Checksum: 281
Coasting Arc #6 (Orbit 1572)
---------------------------------------
Vector Time (GMT): 2012/154/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 941021
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 502638
62 A = 6771776
74 meter
Y = -4205525
31 meter E =
0010516
Z = 5277693
41 I = 51
52362
XDOT = 7501
457977 Wp = 36
42490
YDOT = 1547
569046 meter/sec RA = 194
78848 deg
ZDOT = 526
512123 TA = 48
59474
MA = 48
50440
Ha = 220
842 n
mi
Hp = 209
487
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1649076
84 X = 523989
99
Y = -13797655
23 feet Y = -4199785
78 meter
Z = 17315267
08 Z = 5280186
58
XDOT = 24611
082603 XDOT = 7481
037490
YDOT = 5077
326266 feet/sec YDOT = 1631
340748 meter/sec
ZDOT = 1727
401977 ZDOT = 562
905137
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12496005
61 X = -3808782
51
Y = -6047914
49 feet Y = -1843404
34 meter
Z = 17325870
61 Z = 5280925
36
XDOT = 12535
387984 XDOT = 3820
786258
YDOT = -20595
944312 feet/sec YDOT = -6277
643826 meter/sec
ZDOT = 1876
994514 ZDOT = 572
107928
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 12154
54917593
00016717 00000-0 10270-3 0 9058
2 25544 51
6368 195
6042 0010278 20
4954 339
6610 15
56078403 15733
Satellite: ISS
Catalog Number: 25544
Epoch time: 12154
54917593 = yrday
fracday
Element set: 905
Inclination: 51
6368 deg
RA of node: 195
6042 deg
Eccentricity:
0010278
Arg of perigee: 20
4954 deg
Mean anomaly: 339
6610 deg
Mean motion: 15
56078403 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1573
Checksum: 315
Coasting Arc #7 (Orbit 1587)
---------------------------------------
Vector Time (GMT): 2012/155/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 941021
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2998906
44 A = 6773107
98 meter
Y = 3494507
76 meter E =
0017551
Z = -4979183
63 I = 51
55820
XDOT = -6791
928443 Wp = 69
83274
YDOT = -2857
569244 meter/sec RA = 189
76148 deg
ZDOT = 2097
117541 TA = 220
55775
MA = 220
68865
Ha = 220
979 n
mi
Hp = 209
231
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9838931
90 X = -3013571
73
Y = 11464920
47 feet Y = 3460890
90 meter
Z = -16335904
31 Z = -4993787
50
XDOT = -22283
229799 XDOT = -6769
657203
YDOT = -9375
227178 feet/sec YDOT = -2933
396587 meter/sec
ZDOT = 6880
306892 ZDOT = 2064
175803
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7790793
01 X = 2374633
71
Y = 12867640
85 feet Y = 3922056
93 meter
Z = -16396283
58 Z = -4997587
23
XDOT = -15022
143320 XDOT = -4578
749284
YDOT = 17640
243508 feet/sec YDOT = 5376
746221 meter/sec
ZDOT = 6745
003946 ZDOT = 2055
877203
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 12155
51249930
00016717 00000-0 10270-3 0 9060
2 25544 51
6372 190
7871 0010376 23
7209 336
4421 15
56066825 15888
Satellite: ISS
Catalog Number: 25544
Epoch time: 12155
51249930 = yrday
fracday
Element set: 906
Inclination: 51
6372 deg
RA of node: 190
7871 deg
Eccentricity:
0010376
Arg of perigee: 23
7209 deg
Mean anomaly: 336
4421 deg
Mean motion: 15
56066825 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1588
Checksum: 312
Coasting Arc #8 (Orbit 1603)
---------------------------------------
Vector Time (GMT): 2012/156/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 941021
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5130200
43 A = 6777727
28 meter
Y = -2485310
21 meter E =
0019549
Z = 3661118
92 I = 51
60305
XDOT = 4997
205758 Wp = 58
53958
YDOT = 3871
885650 meter/sec RA = 184
74828 deg
ZDOT = -4346
904165 TA = 77
86850
MA = 77
64956
Ha = 220
977 n
mi
Hp = 208
989
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16831366
25 X = 5139825
33
Y = -8153904
88 feet Y = -2427887
95 meter
Z = 12011545
01 Z = 3686064
40
XDOT = 16395
032015 XDOT = 4974
654622
YDOT = 12703
036909 feet/sec YDOT = 3927
642154 meter/sec
ZDOT = -14261
496605 ZDOT = -4322
681830
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2745752
53 X = -836905
37
Y = -18432585
25 feet Y = -5618251
98 meter
Z = 12114409
28 Z = 3692471
95
XDOT = 15720
316030 XDOT = 4791
552326
YDOT = -11707
467694 feet/sec YDOT = -3568
436153 meter/sec
ZDOT = -14162
141065 ZDOT = -4316
620597
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 12156
54003068
00016717 00000-0 10270-3 0 9075
2 25544 51
6358 185
6484 0010473 27
8821 332
2892 15
56129424 16048
Satellite: ISS
Catalog Number: 25544
Epoch time: 12156
54003068 = yrday
fracday
Element set: 907
Inclination: 51
6358 deg
RA of node: 185
6484 deg
Eccentricity:
0010473
Arg of perigee: 27
8821 deg
Mean anomaly: 332
2892 deg
Mean motion: 15
56129424 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1604
Checksum: 307
Coasting Arc #9 (Orbit 1618)
---------------------------------------
Vector Time (GMT): 2012/157/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 941021
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6429174
11 A = 6782214
82 meter
Y = 1342359
57 meter E =
0018060
Z = -1662127
91 I = 51
64944
XDOT = -2409
549657 Wp = 35
01421
YDOT = -4514
788799 meter/sec RA = 179
75675 deg
ZDOT = 5719
232581 TA = 306
75540
MA = 306
92108
Ha = 220
997 n
mi
Hp = 208
818
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21093090
91 X = -6435632
54
Y = 4404066
82 feet Y = 1270428
75 meter
Z = -5453175
55 Z = -1693376
12
XDOT = -7905
346645 XDOT = -2386
668120
YDOT = -14812
299209 feet/sec YDOT = -4541
606946 meter/sec
ZDOT = 18763
886419 ZDOT = 5707
581834
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1753576
12 X = -534490
00
Y = 21443384
63 feet Y = 6535943
64 meter
Z = -5581902
77 Z = -1701363
97
XDOT = -14914
314033 XDOT = -4545
882917
YDOT = 3614
649852 feet/sec YDOT = 1101
745275 meter/sec
ZDOT = 18716
312867 ZDOT = 5704
732162
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 12157
50333132
00016717 00000-0 10270-3 0 9081
2 25544 51
6365 180
8314 0010413 32
0185 328
1600 15
56153578 16194
Satellite: ISS
Catalog Number: 25544
Epoch time: 12157
50333132 = yrday
fracday
Element set: 908
Inclination: 51
6365 deg
RA of node: 180
8314 deg
Eccentricity:
0010413
Arg of perigee: 32
0185 deg
Mean anomaly: 328
1600 deg
Mean motion: 15
56153578 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1619
Checksum: 279
Coasting Arc #10 (Orbit 1634)
---------------------------------------
Vector Time (GMT): 2012/158/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 941021
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6745039
75 A = 6783283
61 meter
Y = -35686
97 meter E =
0012933
Z = -731870
11 I = 51
68226
XDOT = -611
224868 Wp = 88
38455
YDOT = 4783
050555 meter/sec RA = 174
77797 deg
ZDOT = -5957
020330 TA = 99
51792
MA = 99
37174
Ha = 221
193 n
mi
Hp = 208
722
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22129395
52 X = 6748492
76
Y = -117083
22 feet Y = 39759
67 meter
Z = -2401148
64 Z = -699094
68
XDOT = -2005
330933 XDOT = -635
726683
YDOT = 15692
423081 feet/sec YDOT = 4776
079462 meter/sec
ZDOT = -19544
029954 ZDOT = -5960
048341
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5804770
56 X = 1769294
07
Y = -21369563
35 feet Y = -6513442
91 meter
Z = -2266223
74 Z = -690745
00
XDOT = 13058
102393 XDOT = 3980
109609
YDOT = 5587
645884 feet/sec YDOT = 1703
114466 meter/sec
ZDOT = -19556
897125 ZDOT = -5960
942244
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 12158
53083911
00016717 00000-0 10270-3 0 9093
2 25544 51
6356 175
6919 0010489 35
6158 324
5694 15
56137657 16350
Satellite: ISS
Catalog Number: 25544
Epoch time: 12158
53083911 = yrday
fracday
Element set: 909
Inclination: 51
6356 deg
RA of node: 175
6919 deg
Eccentricity:
0010489
Arg of perigee: 35
6158 deg
Mean anomaly: 324
5694 deg
Mean motion: 15
56137657 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1635
Checksum: 337
Coasting Arc #11 (Orbit 1650)
---------------------------------------
Vector Time (GMT): 2012/159/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 941021
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5963008
60 A = 6779881
21 meter
Y = -1279221
08 meter E =
0022250
Z = 2931737
61 I = 51
70081
XDOT = 3478
343052 Wp = 63
09382
YDOT = -4656
900403 meter/sec RA = 169
79677 deg
ZDOT = 5023
364891 TA = 330
41530
MA = 330
54100
Ha = 221
325 n
mi
Hp = 208
558
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19563676
51 X = -5962502
55
Y = -4196919
56 feet Y = -1345900
74 meter
Z = 9618561
72 Z = 2902770
76
XDOT = 11411
886655 XDOT = 3505
756695
YDOT = -15278
544630 feet/sec YDOT = -4617
850891 meter/sec
ZDOT = 16480
855943 ZDOT = 5040
328336
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8980188
59 X = -2737161
48
Y = 17943961
76 feet Y = 5469319
54 meter
Z = 9499407
93 Z = 2895419
54
XDOT = -10646
473217 XDOT = -3245
045037
YDOT = -14124
326717 feet/sec YDOT = -4305
094783 meter/sec
ZDOT = 16551
087847 ZDOT = 5044
771576
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 12159
55833445
00016717 00000-0 10270-3 0 9103
2 25544 51
6353 170
5534 0010576 38
9292 321
2621 15
56154265 16512
Satellite: ISS
Catalog Number: 25544
Epoch time: 12159
55833445 = yrday
fracday
Element set: 910
Inclination: 51
6353 deg
RA of node: 170
5534 deg
Eccentricity:
0010576
Arg of perigee: 38
9292 deg
Mean anomaly: 321
2621 deg
Mean motion: 15
56154265 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1651
Checksum: 299
Coasting Arc #12 (Orbit 1665)
---------------------------------------
Vector Time (GMT): 2012/160/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 941021
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4270540
65 A = 6774561
00 meter
Y = 2596799
36 meter E =
0019916
Z = -4593086
38 I = 51
71314
XDOT = -5738
730238 Wp = 56
07473
YDOT = 4049
830701 meter/sec RA = 164
79922 deg
ZDOT = -3044
706480 TA = 183
47369
MA = 183
48754
Ha = 221
263 n
mi
Hp = 208
494
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14010960
13 X = 4263497
35
Y = 8519682
94 feet Y = 2644516
39 meter
Z = -15069181
05 Z = -4572357
18
XDOT = -18827
855112 XDOT = -5768
799346
YDOT = 13286
846133 feet/sec YDOT = 3985
488930 meter/sec
ZDOT = -9989
194489 ZDOT = -3072
657335
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11581473
86 X = 3530033
23
Y = -11718368
57 feet Y = -3571758
74 meter
Z = -14984042
16 Z = -4567136
05
XDOT = 7672
769374 XDOT = 2338
660105
YDOT = 20509
489341 feet/sec YDOT = 6251
292351 meter/sec
ZDOT = -10104
626306 ZDOT = -3079
890098
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
52159937
00016717 00000-0 10270-3 0 9110
2 25544 51
6354 165
7355 0010544 42
3969 317
7998 15
56174064 16667
Satellite: ISS
Catalog Number: 25544
Epoch time: 12160
52159937 = yrday
fracday
Element set: 911
Inclination: 51
6354 deg
RA of node: 165
7355 deg
Eccentricity:
0010544
Arg of perigee: 42
3969 deg
Mean anomaly: 317
7998 deg
Mean motion: 15
56174064 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1666
Checksum: 331
Coasting Arc #13 (Orbit 1681)
---------------------------------------
Vector Time (GMT): 2012/161/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 941021
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1930126
04 A = 6771417
68 meter
Y = -3740541
31 meter E =
0011960
Z = 5295067
23 I = 51
73150
XDOT = 7058
968942 Wp = 58
17574
YDOT = -2990
702436 meter/sec RA = 159
78613 deg
ZDOT = 465
799901 TA = 27
42552
MA = 27
36244
Ha = 221
344 n
mi
Hp = 208
260
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6332434
51 X = -1913877
20
Y = -12272117
16 feet Y = -3762034
89 meter
Z = 17372267
82 Z = 5285729
88
XDOT = 23159
346924 XDOT = 7089
624208
YDOT = -9812
015865 feet/sec YDOT = -2911
593321 meter/sec
ZDOT = 1528
214898 ZDOT = 500
166032
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13376370
84 X = -4077117
83
Y = 3619526
09 feet Y = 1103231
55 meter
Z = 17334128
47 Z = 5283442
36
XDOT = -4286
141163 XDOT = -1306
415826
YDOT = -23752
586880 feet/sec YDOT = -7239
788481 meter/sec
ZDOT = 1669
989555 ZDOT = 509
012816
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
54906994
00016717 00000-0 10270-3 0 9127
2 25544 51
6348 160
5961 0010563 45
7805 314
4214 15
56193717 16822
Satellite: ISS
Catalog Number: 25544
Epoch time: 12161
54906994 = yrday
fracday
Element set: 912
Inclination: 51
6348 deg
RA of node: 160
5961 deg
Eccentricity:
0010563
Arg of perigee: 45
7805 deg
Mean anomaly: 314
4214 deg
Mean motion: 15
56193717 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1682
Checksum: 313
Coasting Arc #14 (Orbit 1696)
---------------------------------------
Vector Time (GMT): 2012/162/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 941021
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -579481
87 A = 6772905
65 meter
Y = 4592976
68 meter E =
0020276
Z = -4959863
66 I = 51
76489
XDOT = -7185
940242 Wp = 80
30315
YDOT = 1463
969570 meter/sec RA = 154
77305 deg
ZDOT = 2206
249231 TA = 211
15312
MA = 211
27347
Ha = 221
349 n
mi
Hp = 208
131
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1901187
22 X = -606704
56
Y = 15068821
12 feet Y = 4586344
81 meter
Z = -16272518
56 Z = -4962744
44
XDOT = -23575
919429 XDOT = -7212
494005
YDOT = 4803
049769 feet/sec YDOT = 1383
463258 meter/sec
ZDOT = 7238
350495 ZDOT = 2171
275978
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14401215
21 X = 4389490
39
Y = 4784354
18 feet Y = 1458271
15 meter
Z = -16284768
92 Z = -4963597
57
XDOT = 322
624170 XDOT = 98
335847
YDOT = 23052
933104 feet/sec YDOT = 7026
534010 meter/sec
ZDOT = 7094
189406 ZDOT = 2162
308931
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
51231181
00016717 00000-0 10270-3 0 9135
2 25544 51
6350 155
7791 0010583 48
9005 311
3061 15
56189336 16975
Satellite: ISS
Catalog Number: 25544
Epoch time: 12162
51231181 = yrday
fracday
Element set: 913
Inclination: 51
6350 deg
RA of node: 155
7791 deg
Eccentricity:
0010583
Arg of perigee: 48
9005 deg
Mean anomaly: 311
3061 deg
Mean motion: 15
56189336 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1697
Checksum: 294
Coasting Arc #15 (Orbit 1712)
---------------------------------------
Vector Time (GMT): 2012/163/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 941021
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2930233
69 A = 6777702
35 meter
Y = -4954846
16 meter E =
0021582
Z = 3566900
37 I = 51
80813
XDOT = 6224
155074 Wp = 70
88775
YDOT = 442
742148 meter/sec RA = 149
77345 deg
ZDOT = -4469
234841 TA = 67
03217
MA = 66
80461
Ha = 221
262 n
mi
Hp = 207
965
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9613627
58 X = 2968094
80
Y = -16256056
95 feet Y = -4921867
09 meter
Z = 11702429
02 Z = 3581226
85
XDOT = 20420
456279 XDOT = 6240
452191
YDOT = 1452
566101 feet/sec YDOT = 512
436021 meter/sec
ZDOT = -14662
843967 ZDOT = -4438
958530
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14228622
37 X = -4336884
10
Y = -12362567
94 feet Y = -3768110
71 meter
Z = 11761857
30 Z = 3585014
11
XDOT = 4288
476226 XDOT = 1307
127554
YDOT = -18857
396715 feet/sec YDOT = -5747
734519 meter/sec
ZDOT = -14538
177210 ZDOT = -4431
236414
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
53975644
00016717 00000-0 10270-3 0 9148
2 25544 51
6344 150
6394 0010585 52
0463 308
1645 15
56251125 17134
Satellite: ISS
Catalog Number: 25544
Epoch time: 12163
53975644 = yrday
fracday
Element set: 914
Inclination: 51
6344 deg
RA of node: 150
6394 deg
Eccentricity:
0010585
Arg of perigee: 52
0463 deg
Mean anomaly: 308
1645 deg
Mean motion: 15
56251125 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1713
Checksum: 296
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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