[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
July 25th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 9687 52 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
There are no maneuvers
Coasting Arc #1 (Orbit 2376)
---------------------------------------
Vector Time (GMT): 2012/206/04:30:21
586
Vector Time (MET): N/A
Weight (LBS) : 923981
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2598749
21 A = 6787576
27 meter
Y = -6233980
40 meter E =
0010845
Z = -615367
11 I = 51
34966
XDOT = 4646
203171 Wp = 33
37774
YDOT = 1355
371440 meter/sec RA = 296
80827 deg
ZDOT = 5949
658622 TA = 319
95036
MA = 320
03027
Ha = 219
775 n
mi
Hp = 214
174
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8526080
08 X = 2671255
00
Y = -20452691
61 feet Y = -6204514
15 meter
Z = -2018920
95 Z = -602566
74
XDOT = 15243
448724 XDOT = 4601
800028
YDOT = 4446
756694 feet/sec YDOT = 1407
079694 meter/sec
ZDOT = 19519
877370 ZDOT = 5972
121617
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5199293
48 X = 1584744
65
Y = -21544997
59 feet Y = -6566915
26 meter
Z = -1965478
00 Z = -599077
70
XDOT = 14065
657369 XDOT = 4287
212366
YDOT = 1623
309433 feet/sec YDOT = 494
784715 meter/sec
ZDOT = 19612
354393 ZDOT = 5977
845619
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 12206
18890767
00016717 00000-0 10270-3 0 9004
2 25544 51
6412 297
4818 0001371 309
2143 50
8889 15
54678689 23770
Satellite: ISS
Catalog Number: 25544
Epoch time: 12206
18890767 = yrday
fracday
Element set: 900
Inclination: 51
6412 deg
RA of node: 297
4818 deg
Eccentricity:
0001371
Arg of perigee: 309
2143 deg
Mean anomaly: 50
8889 deg
Mean motion: 15
54678689 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2377
Checksum: 338
Coasting Arc #2 (Orbit 2392)
---------------------------------------
Vector Time (GMT): 2012/207/04:30:21
586
Vector Time (MET): N/A
Weight (LBS) : 923981
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3406204
65 A = 6786935
99 meter
Y = 5721860
47 meter E =
0007520
Z = -1294746
28 I = 51
33444
XDOT = -3618
122609 Wp = 143
78373
YDOT = -3462
353385 meter/sec RA = 291
81470 deg
ZDOT = -5805
883773 TA = 50
36515
MA = 50
29880
Ha = 219
761 n
mi
Hp = 214
106
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11175212
10 X = -3463644
97
Y = 18772508
09 feet Y = 5683449
06 meter
Z = -4247855
25 Z = -1311432
63
XDOT = -11870
481002 XDOT = -3550
933481
YDOT = -11359
427116 feet/sec YDOT = -3502
437559 meter/sec
ZDOT = -19048
175108 ZDOT = -5823
297272
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7692494
92 X = -2344672
45
Y = 20433391
42 feet Y = 6228097
70 meter
Z = -4317260
34 Z = -1315900
95
XDOT = -12070
310971 XDOT = -3679
030784
YDOT = -8567
889724 feet/sec YDOT = -2611
492788 meter/sec
ZDOT = -19119
610195 ZDOT = -5827
657187
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 12207
21736470
00016717 00000-0 10270-3 0 9010
2 25544 51
6407 292
3502 0001341 313
1192 46
9849 15
54698147 23934
Satellite: ISS
Catalog Number: 25544
Epoch time: 12207
21736470 = yrday
fracday
Element set: 901
Inclination: 51
6407 deg
RA of node: 292
3502 deg
Eccentricity:
0001341
Arg of perigee: 313
1192 deg
Mean anomaly: 46
9849 deg
Mean motion: 15
54698147 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2393
Checksum: 298
Coasting Arc #3 (Orbit 2408)
---------------------------------------
Vector Time (GMT): 2012/208/04:30:21
586
Vector Time (MET): N/A
Weight (LBS) : 923981
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3920688
10 A = 6783644
99 meter
Y = -4635852
31 meter E =
0012228
Z = 3012329
42 I = 51
31271
XDOT = 2506
529262 Wp = 78
85355
YDOT = 5326
483752 meter/sec RA = 286
81243 deg
ZDOT = 4920
187068 TA = 315
85412
MA = 315
95165
Ha = 219
635 n
mi
Hp = 214
049
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12863149
95 X = 3957602
62
Y = -15209489
22 feet Y = -4591802
52 meter
Z = 9882970
53 Z = 3031465
24
XDOT = 8223
521201 XDOT = 2422
880088
YDOT = 17475
340395 feet/sec YDOT = 5354
045317 meter/sec
ZDOT = 16142
346022 ZDOT = 4932
160755
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9646368
81 X = 2940213
21
Y = -17382787
18 feet Y = -5298273
53 meter
Z = 9962357
86 Z = 3036526
68
XDOT = 10059
563333 XDOT = 3066
154904
YDOT = 14889
250208 feet/sec YDOT = 4538
243463 meter/sec
ZDOT = 16191
159462 ZDOT = 4935
065404
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 12208
24581069
00016717 00000-0 10270-3 0 9027
2 25544 51
6400 287
2169 0001351 311
8561 48
2477 15
54738296 24095
Satellite: ISS
Catalog Number: 25544
Epoch time: 12208
24581069 = yrday
fracday
Element set: 902
Inclination: 51
6400 deg
RA of node: 287
2169 deg
Eccentricity:
0001351
Arg of perigee: 311
8561 deg
Mean anomaly: 48
2477 deg
Mean motion: 15
54738296 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2409
Checksum: 306
Coasting Arc #4 (Orbit 2423)
---------------------------------------
Vector Time (GMT): 2012/209/04:30:21
586
Vector Time (MET): N/A
Weight (LBS) : 923981
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4210682
45 A = 6779372
61 meter
Y = 3038681
64 meter E =
0008747
Z = -4367664
16 I = 51
29004
XDOT = -1359
229778 Wp = 61
34079
YDOT = -6739
749018 meter/sec RA = 281
79844 deg
ZDOT = -3379
663432 TA = 174
23890
MA = 174
22883
Ha = 219
813 n
mi
Hp = 213
840
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13814574
97 X = -4223131
64
Y = 9969427
94 feet Y = 2991525
92 meter
Z = -14329606
84 Z = -4388149
37
XDOT = -4459
415283 XDOT = -1267
345931
YDOT = -22112
037459 feet/sec YDOT = -6754
434739 meter/sec
ZDOT = -11088
134619 ZDOT = -3386
043852
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11343645
91 X = -3457543
27
Y = 12614144
02 feet Y = 3844791
10 meter
Z = -14414391
25 Z = -4393506
45
XDOT = -7990
673136 XDOT = -2435
557172
YDOT = -19881
811672 feet/sec YDOT = -6059
976198 meter/sec
ZDOT = -11113
743113 ZDOT = -3387
468901
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 12209
20997213
00016717 00000-0 10270-3 0 9037
2 25544 51
6394 282
4055 0001254 325
8118 34
2955 15
54740790 24248
Satellite: ISS
Catalog Number: 25544
Epoch time: 12209
20997213 = yrday
fracday
Element set: 903
Inclination: 51
6394 deg
RA of node: 282
4055 deg
Eccentricity:
0001254
Arg of perigee: 325
8118 deg
Mean anomaly: 34
2955 deg
Mean motion: 15
54740790 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2424
Checksum: 299
Coasting Arc #5 (Orbit 2439)
---------------------------------------
Vector Time (GMT): 2012/210/04:30:21
586
Vector Time (MET): N/A
Weight (LBS) : 923981
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4278194
36 A = 6776329
74 meter
Y = -1101761
61 meter E =
0003399
Z = 5135916
16 I = 51
27418
XDOT = 244
496532 Wp = 115
56774
YDOT = 7536
770712 meter/sec RA = 276
77136 deg
ZDOT = 1410
956810 TA = 320
78416
MA = 320
80878
Ha = 219
769 n
mi
Hp = 213
978
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14036070
73 X = 4265247
57
Y = -3614703
44 feet Y = -1053993
10 meter
Z = 16850118
62 Z = 5156667
73
XDOT = 802
153975 XDOT = 153
346578
YDOT = 24726
938032 feet/sec YDOT = 7538
995032 meter/sec
ZDOT = 4629
123391 ZDOT = 1411
923927
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12758947
00 X = 3888927
04
Y = -6662708
46 feet Y = -2030793
54 meter
Z = 16935803
72 Z = 5162032
98
XDOT = 5844
663925 XDOT = 1781
453564
YDOT = 22985
282753 feet/sec YDOT = 7005
914183 meter/sec
ZDOT = 4632
334083 ZDOT = 1411
935428
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 12210
23840188
00016717 00000-0 10270-3 0 9041
2 25544 51
6393 277
2727 0001273 331
0044 29
1038 15
54704640 24400
Satellite: ISS
Catalog Number: 25544
Epoch time: 12210
23840188 = yrday
fracday
Element set: 904
Inclination: 51
6393 deg
RA of node: 277
2727 deg
Eccentricity:
0001273
Arg of perigee: 331
0044 deg
Mean anomaly: 29
1038 deg
Mean motion: 15
54704640 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2440
Checksum: 275
Coasting Arc #6 (Orbit 2454)
---------------------------------------
Vector Time (GMT): 2012/211/04:30:21
586
Vector Time (MET): N/A
Weight (LBS) : 923981
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4183779
95 A = 6775707
32 meter
Y = -979230
19 meter E =
0014025
Z = -5251249
07 I = 51
27000
XDOT = 832
472817 Wp = 91
91774
YDOT = -7576
737385 meter/sec RA = 271
73841 deg
ZDOT = 750
911227 TA = 185
29461
MA = 185
30946
Ha = 219
858 n
mi
Hp = 213
690
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13726312
16 X = -4147009
95
Y = -3212697
46 feet Y = -1025809
62 meter
Z = -17228507
45 Z = -5271484
26
XDOT = 2731
210030 XDOT = 913
487866
YDOT = -24858
062287 feet/sec YDOT = -7566
975262 meter/sec
ZDOT = 2463
619511 ZDOT = 755
151222
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13993614
26 X = -4265253
63
Y = 181528
96 feet Y = 55330
03 meter
Z = -17311855
66 Z = -5276653
61
XDOT = -3373
370762 XDOT = -1028
203408
YDOT = -23755
028279 feet/sec YDOT = -7240
532619 meter/sec
ZDOT = 2481
878286 ZDOT = 756
476501
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 12211
20254377
00016717 00000-0 10270-3 0 9059
2 25544 51
6393 272
4611 0001124 334
1112 25
9984 15
54760250 24553
Satellite: ISS
Catalog Number: 25544
Epoch time: 12211
20254377 = yrday
fracday
Element set: 905
Inclination: 51
6393 deg
RA of node: 272
4611 deg
Eccentricity:
0001124
Arg of perigee: 334
1112 deg
Mean anomaly: 25
9984 deg
Mean motion: 15
54760250 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2455
Checksum: 276
Coasting Arc #7 (Orbit 2470)
---------------------------------------
Vector Time (GMT): 2012/212/04:30:21
586
Vector Time (MET): N/A
Weight (LBS) : 923981
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3912540
33 A = 6778208
68 meter
Y = 2983956
72 meter E =
0008151
Z = 4658071
50 I = 51
27791
XDOT = -1873
920841 Wp = 55
62206
YDOT = 6881
286074 meter/sec RA = 266
70867 deg
ZDOT = -2826
077621 TA = 62
59542
MA = 62
51252
Ha = 219
786 n
mi
Hp = 213
843
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12836418
40 X = 3856254
84
Y = 9789884
25 feet Y = 3027393
95 meter
Z = 15282386
80 Z = 4676941
75
XDOT = -6148
034256 XDOT = -1937
001305
YDOT = 22576
397880 feet/sec YDOT = 6859
978339 meter/sec
ZDOT = -9271
908205 ZDOT = -2835
333350
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14843182
67 X = 4524202
08
Y = 6157908
37 feet Y = 1876930
47 meter
Z = 15359912
43 Z = 4681701
31
XDOT = 410
405349 XDOT = 125
091550
YDOT = 22300
696224 feet/sec YDOT = 6797
252209 meter/sec
ZDOT = -9310
773840 ZDOT = -2837
923867
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 12212
23095386
00016717 00000-0 10270-3 0 9067
2 25544 51
6388 267
3288 0001152 335
9213 24
1885 15
54750936 24711
Satellite: ISS
Catalog Number: 25544
Epoch time: 12212
23095386 = yrday
fracday
Element set: 906
Inclination: 51
6388 deg
RA of node: 267
3288 deg
Eccentricity:
0001152
Arg of perigee: 335
9213 deg
Mean anomaly: 24
1885 deg
Mean motion: 15
54750936 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2471
Checksum: 312
Coasting Arc #8 (Orbit 2485)
---------------------------------------
Vector Time (GMT): 2012/213/04:30:21
586
Vector Time (MET): N/A
Weight (LBS) : 923981
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3491614
02 A = 6782241
88 meter
Y = -4668223
70 meter E =
0004809
Z = -3469688
95 I = 51
29509
XDOT = 2857
337422 Wp = 81
33323
YDOT = -5491
395072 meter/sec RA = 261
68969 deg
ZDOT = 4518
988922 TA = 237
71735
MA = 237
76395
Ha = 219
864 n
mi
Hp = 213
660
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11455426
57 X = -3422298
87
Y = -15315694
55 feet Y = -4706881
20 meter
Z = -11383493
94 Z = -3486482
79
XDOT = 9374
466607 XDOT = 2896
579210
YDOT = -18016
388033 feet/sec YDOT = -5459
223578 meter/sec
ZDOT = 14826
079140 ZDOT = 4532
964225
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15164452
88 X = -4622125
24
Y = -11587294
89 feet Y = -3531807
48 meter
Z = -11452301
00 Z = -3490661
34
XDOT = 3116
635845 XDOT = 949
950606
YDOT = -18770
002878 feet/sec YDOT = -5721
096877 meter/sec
ZDOT = 14884
264827 ZDOT = 4536
723919
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 12213
19507943
00016717 00000-0 10270-3 0 9071
2 25544 51
6394 262
5172 0001069 344
3074 15
8045 15
54788288 24865
Satellite: ISS
Catalog Number: 25544
Epoch time: 12213
19507943 = yrday
fracday
Element set: 907
Inclination: 51
6394 deg
RA of node: 262
5172 deg
Eccentricity:
0001069
Arg of perigee: 344
3074 deg
Mean anomaly: 15
8045 deg
Mean motion: 15
54788288 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2486
Checksum: 320
Coasting Arc #9 (Orbit 2501)
---------------------------------------
Vector Time (GMT): 2012/214/04:30:21
586
Vector Time (MET): N/A
Weight (LBS) : 923981
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2863910
73 A = 6785971
07 meter
Y = 5879443
82 meter E =
0013204
Z = 1789146
81 I = 51
31207
XDOT = -3790
625440 Wp = 110
41717
YDOT = 3569
466250 meter/sec RA = 256
68406 deg
ZDOT = -5632
874035 TA = 49
82395
MA = 49
70842
Ha = 219
835 n
mi
Hp = 213
689
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9396032
59 X = 2789261
67
Y = 19289513
83 feet Y = 5911052
32 meter
Z = 5869904
24 Z = 1802878
35
XDOT = -12436
435172 XDOT = -3802
895662
YDOT = 11710
847277 feet/sec YDOT = 3527
008944 meter/sec
ZDOT = -18480
557857 ZDOT = -5651
317804
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14584278
48 X = 4445288
08
Y = 15716493
14 feet Y = 4790387
11 meter
Z = 5925977
79 Z = 1806238
03
XDOT = -7221
298932 XDOT = -2201
051915
YDOT = 13733
979866 feet/sec YDOT = 4186
117063 meter/sec
ZDOT = -18556
983218 ZDOT = -5656
168485
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 12214
22347006
00016717 00000-0 10270-3 0 9089
2 25544 51
6383 257
3848 0001205 343
6799 16
4315 15
54808617 25028
Satellite: ISS
Catalog Number: 25544
Epoch time: 12214
22347006 = yrday
fracday
Element set: 908
Inclination: 51
6383 deg
RA of node: 257
3848 deg
Eccentricity:
0001205
Arg of perigee: 343
6799 deg
Mean anomaly: 16
4315 deg
Mean motion: 15
54808617 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2502
Checksum: 301
Coasting Arc #10 (Orbit 2517)
---------------------------------------
Vector Time (GMT): 2012/215/04:30:21
586
Vector Time (MET): N/A
Weight (LBS) : 923981
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2052379
04 A = 6787304
76 meter
Y = -6461865
37 meter E =
0012962
Z = 102330
08 I = 51
32559
XDOT = 4598
413838 Wp = 42
89669
YDOT = -1358
757413 meter/sec RA = 251
68723 deg
ZDOT = 5987
442169 TA = 318
21092
MA = 318
30983
Ha = 219
888 n
mi
Hp = 213
594
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6733527
05 X = -1980465
68
Y = -21200345
70 feet Y = -6484414
26 meter
Z = 335728
62 Z = 92534
31
XDOT = 15086
659575 XDOT = 4584
181079
YDOT = -4457
865528 feet/sec YDOT = -1307
414984 meter/sec
ZDOT = 19643
839137 ZDOT = 6009
745848
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12944995
85 X = -3945634
74
Y = -18089976
96 feet Y = -5513824
98 meter
Z = 295929
12 Z = 90199
20
XDOT = 11543
404990 XDOT = 3518
429841
YDOT = -7910
775061 feet/sec YDOT = -2411
204239 meter/sec
ZDOT = 19735
976301 ZDOT = 6015
525576
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 12215
25185248
00016717 00000-0 10270-3 0 9092
2 25544 51
6393 252
2524 0001045 355
0474 5
0669 15
54824900 25189
Satellite: ISS
Catalog Number: 25544
Epoch time: 12215
25185248 = yrday
fracday
Element set: 909
Inclination: 51
6393 deg
RA of node: 252
2524 deg
Eccentricity:
0001045
Arg of perigee: 355
0474 deg
Mean anomaly: 5
0669 deg
Mean motion: 15
54824900 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2518
Checksum: 295
Coasting Arc #11 (Orbit 2532)
---------------------------------------
Vector Time (GMT): 2012/216/04:30:21
586
Vector Time (MET): N/A
Weight (LBS) : 923981
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 998255
19 A = 6785525
69 meter
Y = 6399497
66 meter E =
0005816
Z = -2018638
82 I = 51
32981
XDOT = -5222
433616 Wp = 132
43616
YDOT = -926
781396 meter/sec RA = 246
69030 deg
ZDOT = -5534
752925 TA = 69
96610
MA = 69
90349
Ha = 219
916 n
mi
Hp = 213
532
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3275115
44 X = 936426
35
Y = 20995727
22 feet Y = 6410315
12 meter
Z = -6622830
76 Z = -2013939
45
XDOT = -17133
968557 XDOT = -5184
796084
YDOT = -3040
621377 feet/sec YDOT = -984
971292 meter/sec
ZDOT = -18158
638204 ZDOT = -5560
031267
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9953066
65 X = 3033694
71
Y = 18781161
37 feet Y = 5724497
98 meter
Z = -6604034
54 Z = -2012909
73
XDOT = -15718
439074 XDOT = -4790
980230
YDOT = 1924
484742 feet/sec YDOT = 586
582949 meter/sec
ZDOT = -18262
838893 ZDOT = -5566
513294
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
21595174
00016717 00000-0 10270-3 0 9104
2 25544 51
6387 247
4404 0001208 359
0085 1
1065 15
54844488 25335
Satellite: ISS
Catalog Number: 25544
Epoch time: 12216
21595174 = yrday
fracday
Element set: 910
Inclination: 51
6387 deg
RA of node: 247
4404 deg
Eccentricity:
0001208
Arg of perigee: 359
0085 deg
Mean anomaly: 1
1065 deg
Mean motion: 15
54844488 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2533
Checksum: 293
Coasting Arc #12 (Orbit 2548)
---------------------------------------
Vector Time (GMT): 2012/217/04:30:21
586
Vector Time (MET): N/A
Weight (LBS) : 923981
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 227042
76 A = 6781561
01 meter
Y = -5713275
24 meter E =
0011843
Z = 3635998
35 I = 51
33050
XDOT = 5566
952479 Wp = 89
18237
YDOT = 2996
162912 meter/sec RA = 241
68481 deg
ZDOT = 4348
155086 TA = 314
23284
MA = 314
33002
Ha = 219
843 n
mi
Hp = 213
502
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 744890
94 X = 273250
42
Y = -18744341
32 feet Y = -5710477
97 meter
Z = 11929128
44 Z = 3637213
47
XDOT = 18264
279787 XDOT = 5511
913113
YDOT = 9829
930813 feet/sec YDOT = 3058
108253 meter/sec
ZDOT = 14265
600675 ZDOT = 4375
064856
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5758383
56 X = -1755155
31
Y = -17849768
79 feet Y = -5440609
53 meter
Z = 11934658
45 Z = 3637683
89
XDOT = 19137
720686 XDOT = 5833
177265
YDOT = 3464
975720 feet/sec YDOT = 1056
124599 meter/sec
ZDOT = 14376
352126 ZDOT = 4381
912128
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
24431452
00016717 00000-0 10270-3 0 9117
2 25544 51
6395 242
3078 0001073 358
7095 1
4055 15
54867879 25490
Satellite: ISS
Catalog Number: 25544
Epoch time: 12217
24431452 = yrday
fracday
Element set: 911
Inclination: 51
6395 deg
RA of node: 242
3078 deg
Eccentricity:
0001073
Arg of perigee: 358
7095 deg
Mean anomaly: 1
4055 deg
Mean motion: 15
54867879 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2549
Checksum: 311
Coasting Arc #13 (Orbit 2563)
---------------------------------------
Vector Time (GMT): 2012/218/04:30:21
586
Vector Time (MET): N/A
Weight (LBS) : 923981
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1611443
30 A = 6777450
52 meter
Y = 4526901
90 meter E =
0011916
Z = -4791004
06 I = 51
33242
XDOT = -5513
288649 Wp = 66
60172
YDOT = -4664
431148 meter/sec RA = 236
66755 deg
ZDOT = -2553
347121 TA = 178
12740
MA = 178
12293
Ha = 219
934 n
mi
Hp = 213
408
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5286887
46 X = -1638671
07
Y = 14852040
35 feet Y = 4508729
48 meter
Z = -15718517
24 Z = -4798898
39
XDOT = -18088
217353 XDOT = -5448
316892
YDOT = -15303
251799 feet/sec YDOT = -4725
720902 meter/sec
ZDOT = -8377
123101 ZDOT = -2579
972130
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 453862
62 X = 138337
33
Y = 15725476
47 feet Y = 4793125
23 meter
Z = -15751490
86 Z = -4801054
41
XDOT = -21165
217602 XDOT = -6451
158325
YDOT = -7888
351425 feet/sec YDOT = -2404
369514 meter/sec
ZDOT = -8486
561510 ZDOT = -2586
703948
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
20839725
00016717 00000-0 10270-3 0 9120
2 25544 51
6399 237
4966 0001203 4
3094 355
8069 15
54857564 25641
Satellite: ISS
Catalog Number: 25544
Epoch time: 12218
20839725 = yrday
fracday
Element set: 912
Inclination: 51
6399 deg
RA of node: 237
4966 deg
Eccentricity:
0001203
Arg of perigee: 4
3094 deg
Mean anomaly: 355
8069 deg
Mean motion: 15
54857564 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2564
Checksum: 325
Coasting Arc #14 (Orbit 2579)
---------------------------------------
Vector Time (GMT): 2012/219/04:30:21
586
Vector Time (MET): N/A
Weight (LBS) : 923981
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3014513
24 A = 6775189
43 meter
Y = -2991945
71 meter E =
0002679
Z = 5276325
23 I = 51
34346
XDOT = 5013
426580 Wp = 82
91550
YDOT = 5792
465356 meter/sec RA = 231
63975 deg
ZDOT = 420
452527 TA = 3
06116
MA = 3
05952
Ha = 219
785 n
mi
Hp = 213
410
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9890135
30 X = 3022114
90
Y = -9816094
85 feet Y = -2958193
01 meter
Z = 17310778
30 Z = 5290987
88
XDOT = 16448
249936 XDOT = 4946
238994
YDOT = 19004
151432 feet/sec YDOT = 5848
152946 meter/sec
ZDOT = 1379
437424 ZDOT = 444
643953
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5416256
77 X = 1650875
06
Y = -12756460
55 feet Y = -3888169
18 meter
Z = 17371540
42 Z = 5294845
52
XDOT = 21412
159344 XDOT = 6526
426168
YDOT = 11104
480546 feet/sec YDOT = 3384
645670 meter/sec
ZDOT = 1478
747095 ZDOT = 450
722114
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
23674154
00016717 00000-0 10270-3 0 9138
2 25544 51
6405 232
3632 0001249 5
6732 354
4435 15
54892136 25800
Satellite: ISS
Catalog Number: 25544
Epoch time: 12219
23674154 = yrday
fracday
Element set: 913
Inclination: 51
6405 deg
RA of node: 232
3632 deg
Eccentricity:
0001249
Arg of perigee: 5
6732 deg
Mean anomaly: 354
4435 deg
Mean motion: 15
54892136 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2580
Checksum: 292
Coasting Arc #15 (Orbit 2594)
---------------------------------------
Vector Time (GMT): 2012/220/04:30:21
586
Vector Time (MET): N/A
Weight (LBS) : 923981
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4322236
14 A = 6776105
09 meter
Y = 1316698
27 meter E =
0013381
Z = -5061777
08 I = 51
36677
XDOT = -3993
182782 Wp = 98
13948
YDOT = -6290
540744 meter/sec RA = 226
61305 deg
ZDOT = 1775
613919 TA = 189
11142
MA = 189
13573
Ha = 219
927 n
mi
Hp = 213
169
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14180564
75 X = -4312049
78
Y = 4319876
21 feet Y = 1268421
28 meter
Z = -16606880
19 Z = -5082749
35
XDOT = -13100
993378 XDOT = -3931
169315
YDOT = -20638
257035 feet/sec YDOT = -6334
848255 meter/sec
ZDOT = 5825
504982 ZDOT = 1756
366068
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11290289
35 X = -3441280
19
Y = 9454814
52 feet Y = 2881827
46 meter
Z = -16693533
65 Z = -5088189
06
XDOT = -19439
801960 XDOT = -5925
251637
YDOT = -13079
916379 feet/sec YDOT = -3986
758512 meter/sec
ZDOT = 5746
626320 ZDOT = 1751
571702
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
20080640
00016717 00000-0 10270-3 0 9149
2 25544 51
6408 227
5525 0001242 14
8195 345
2994 15
54906939 25959
Satellite: ISS
Catalog Number: 25544
Epoch time: 12220
20080640 = yrday
fracday
Element set: 914
Inclination: 51
6408 deg
RA of node: 227
5525 deg
Eccentricity:
0001242
Arg of perigee: 14
8195 deg
Mean anomaly: 345
2994 deg
Mean motion: 15
54906939 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2595
Checksum: 302
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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