[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
July 9th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 9149 32 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 102 9 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 423)
---------------------------------------
Vector Time (GMT): 2011/189/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2264086
51 A = 6770736
88 meter
Y = -5952631
29 meter E =
0005971
Z = -2297421
30 I = 51
92808
XDOT = 5402
047817 Wp = 290
51029
YDOT = 53
588089 meter/sec RA = 52
76204 deg
ZDOT = -5449
063495 TA = 275
02356
MA = 275
09172
Ha = 212
377 n
mi
Hp = 207
761
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7428105
34 X = -2186194
36
Y = -19529630
23 feet Y = -5977513
93 meter
Z = -7537471
47 Z = -2308231
61
XDOT = 17723
253994 XDOT = 5427
517524
YDOT = 175
813940 feet/sec YDOT = 114
140054 meter/sec
ZDOT = -17877
504905 ZDOT = -5422
758602
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16888607
70 X = -5147647
63
Y = 12275980
24 feet Y = 3741718
78 meter
Z = -7581023
74 Z = -2310696
04
XDOT = -3642
602336 XDOT = -1110
265192
YDOT = -16012
645190 feet/sec YDOT = -4880
654254 meter/sec
ZDOT = -17770
665676 ZDOT = -5416
498898
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 11189
52743565
00016717 00000-0 10270-3 0 9004
2 25544 51
6399 53
2294 0011517 302
9952 57
0096 15
59757317 4242
Satellite: ISS
Catalog Number: 25544
Epoch time: 11189
52743565 = yrday
fracday
Element set: 900
Inclination: 51
6399 deg
RA of node: 53
2294 deg
Eccentricity:
0011517
Arg of perigee: 302
9952 deg
Mean anomaly: 57
0096 deg
Mean motion: 15
59757317 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 424
Checksum: 320
Coasting Arc #2 (Orbit 439)
---------------------------------------
Vector Time (GMT): 2011/190/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -840600
09 A = 6763149
80 meter
Y = 4683649
10 meter E =
0004395
Z = 4806878
19 I = 51
88357
XDOT = -6167
222661 Wp = 321
54777
YDOT = -3763
693924 meter/sec RA = 47
75112 deg
ZDOT = 2593
343490 TA = 103
04694
MA = 102
99787
Ha = 212
705 n
mi
Hp = 207
507
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2757874
30 X = -916261
95
Y = 15366302
83 feet Y = 4673825
34 meter
Z = 15770597
73 Z = 4802611
38
XDOT = -20233
670149 XDOT = -6137
275897
YDOT = -12348
077180 feet/sec YDOT = -3832
492450 meter/sec
ZDOT = 8508
344782 ZDOT = 2563
455471
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15550290
42 X = 4739728
52
Y = -1572576
53 feet Y = -479321
33 meter
Z = 15752979
31 Z = 4801508
09
XDOT = -6276
537142 XDOT = -1913
088521
YDOT = 21799
763647 feet/sec YDOT = 6644
567960 meter/sec
ZDOT = 8387
180475 ZDOT = 2556
412609
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 11190
55253538
00016717 00000-0 10270-3 0 9016
2 25544 51
6398 48
0741 0011492 308
0053 52
0064 15
59762950 4408
Satellite: ISS
Catalog Number: 25544
Epoch time: 11190
55253538 = yrday
fracday
Element set: 901
Inclination: 51
6398 deg
RA of node: 48
0741 deg
Eccentricity:
0011492
Arg of perigee: 308
0053 deg
Mean anomaly: 52
0064 deg
Mean motion: 15
59762950 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 440
Checksum: 288
Coasting Arc #3 (Orbit 454)
---------------------------------------
Vector Time (GMT): 2011/191/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3911036
73 A = 6761508
68 meter
Y = -1919571
26 meter E =
0006956
Z = -5173924
31 I = 51
85636
XDOT = 4735
628227 Wp = 44
15012
YDOT = 5874
143795 meter/sec RA = 42
70782 deg
ZDOT = 1406
366852 TA = 239
28842
MA = 239
35697
Ha = 212
843 n
mi
Hp = 207
285
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12831485
32 X = 3957344
95
Y = -6297805
97 feet Y = -1875575
96 meter
Z = -16974817
28 Z = -5154812
37
XDOT = 15536
838015 XDOT = 4662
758602
YDOT = 19272
125313 feet/sec YDOT = 5926
692821 meter/sec
ZDOT = 4614
064475 ZDOT = 1429
196343
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9855420
39 X = -3003932
13
Y = -10479196
85 feet Y = -3194059
20 meter
Z = -16897068
37 Z = -5150226
44
XDOT = 13032
853292 XDOT = 3972
413683
YDOT = -19813
986011 feet/sec YDOT = -6039
302936 meter/sec
ZDOT = 4706
420558 ZDOT = 1434
516986
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 11191
51355693
00016717 00000-0 10270-3 0 9029
2 25544 51
6388 43
2411 0011573 310
9897 49
0257 15
59818111 4553
Satellite: ISS
Catalog Number: 25544
Epoch time: 11191
51355693 = yrday
fracday
Element set: 902
Inclination: 51
6388 deg
RA of node: 43
2411 deg
Eccentricity:
0011573
Arg of perigee: 310
9897 deg
Mean anomaly: 49
0257 deg
Mean motion: 15
59818111 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 455
Checksum: 306
Coasting Arc #4 (Orbit 470)
---------------------------------------
Vector Time (GMT): 2011/192/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5809775
70 A = 6768356
76 meter
Y = -1279864
66 meter E =
0008726
Z = 3232558
50 I = 51
85732
XDOT = -1389
414591 Wp = 30
28578
YDOT = -5827
793550 meter/sec RA = 37
68258 deg
ZDOT = -4791
572755 TA = 112
33672
MA = 112
24421
Ha = 212
984 n
mi
Hp = 207
011
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19060943
89 X = -5810735
28
Y = -4199031
03 feet Y = -1344839
02 meter
Z = 10605506
89 Z = 3204332
25
XDOT = -4558
446820 XDOT = -1300
867383
YDOT = -19120
057578 feet/sec YDOT = -5842
834916 meter/sec
ZDOT = -15720
383055 ZDOT = -4798
108401
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2005825
34 X = 611375
57
Y = 19476783
07 feet Y = 5936523
48 meter
Z = 10490939
21 Z = 3197638
27
XDOT = -15338
706444 XDOT = -4675
237724
YDOT = 10084
533789 feet/sec YDOT = 3073
765899 meter/sec
ZDOT = -15746
552731 ZDOT = -4799
549272
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 11192
53863917
00016717 00000-0 10270-3 0 9036
2 25544 51
6394 38
0871 0011810 314
8760 45
1436 15
59860823 4719
Satellite: ISS
Catalog Number: 25544
Epoch time: 11192
53863917 = yrday
fracday
Element set: 903
Inclination: 51
6394 deg
RA of node: 38
0871 deg
Eccentricity:
0011810
Arg of perigee: 314
8760 deg
Mean anomaly: 45
1436 deg
Mean motion: 15
59860823 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 471
Checksum: 309
Coasting Arc #5 (Orbit 486)
---------------------------------------
Vector Time (GMT): 2011/193/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5623792
38 A = 6772834
24 meter
Y = 3750130
55 meter E =
0017263
Z = 150674
47 I = 51
84589
XDOT = -2747
098121 Wp = 4
33047
YDOT = 3875
792969 meter/sec RA = 32
69324 deg
ZDOT = 6040
517767 TA = 357
29352
MA = 357
30285
Ha = 213
195 n
mi
Hp = 206
785
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18450762
39 X = 5580707
78
Y = 12303577
92 feet Y = 3812778
29 meter
Z = 494338
82 Z = 177890
56
XDOT = -9012
789112 XDOT = -2819
577212
YDOT = 12715
856196 feet/sec YDOT = 3844
666914 meter/sec
ZDOT = 19817
971675 ZDOT = 6026
997161
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5534628
88 X = 1686954
88
Y = -21472198
84 feet Y = -6544726
21 meter
Z = 604643
26 Z = 184295
26
XDOT = 13450
528907 XDOT = 4099
721211
YDOT = 4025
607154 feet/sec YDOT = 1227
005060 meter/sec
ZDOT = 19762
796104 ZDOT = 6023
700253
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 11193
56371631
00016717 00000-0 10270-3 0 9048
2 25544 51
6379 32
9314 0011663 318
5764 41
4506 15
59818506 4873
Satellite: ISS
Catalog Number: 25544
Epoch time: 11193
56371631 = yrday
fracday
Element set: 904
Inclination: 51
6379 deg
RA of node: 32
9314 deg
Eccentricity:
0011663
Arg of perigee: 318
5764 deg
Mean anomaly: 41
4506 deg
Mean motion: 15
59818506 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 487
Checksum: 315
Coasting Arc #6 (Orbit 501)
---------------------------------------
Vector Time (GMT): 2011/194/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3276962
94 A = 6767570
19 meter
Y = -4803922
33 meter E =
0009757
Z = -3469475
29 I = 51
80185
XDOT = 6102
184478 Wp = 347
42092
YDOT = -855
411613 meter/sec RA = 27
70073 deg
ZDOT = -4567
452978 TA = 233
26890
MA = 233
35855
Ha = 213
332 n
mi
Hp = 206
482
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10751190
75 X = -3206147
20
Y = -15760900
04 feet Y = -4840170
76 meter
Z = -11382792
94 Z = -3485223
34
XDOT = 20020
290283 XDOT = 6133
483812
YDOT = -2806
468545 feet/sec YDOT = -786
997467 meter/sec
ZDOT = -14985
081949 ZDOT = -4537
733184
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11094380
66 X = -3381567
22
Y = 15474355
50 feet Y = 4716583
56 meter
Z = -11446444
30 Z = -3488876
22
XDOT = -8460
484827 XDOT = -2578
755775
YDOT = -17089
217012 feet/sec YDOT = -5208
793345 meter/sec
ZDOT = -14864
299442 ZDOT = -4530
638470
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 11194
52471698
00016717 00000-0 10270-3 0 9050
2 25544 51
6371 28
0992 0011644 322
4384 37
5957 15
59846100 5029
Satellite: ISS
Catalog Number: 25544
Epoch time: 11194
52471698 = yrday
fracday
Element set: 905
Inclination: 51
6371 deg
RA of node: 28
0992 deg
Eccentricity:
0011644
Arg of perigee: 322
4384 deg
Mean anomaly: 37
5957 deg
Mean motion: 15
59846100 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 502
Checksum: 313
Coasting Arc #7 (Orbit 517)
---------------------------------------
Vector Time (GMT): 2011/195/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -508597
93 A = 6761198
79 meter
Y = 4255898
92 meter E =
0008416
Z = 5230792
13 I = 51
75266
XDOT = -7294
302934 Wp = 335
90163
YDOT = -2150
334394 meter/sec RA = 22
66427 deg
ZDOT = 1048
428924 TA = 104
13024
MA = 104
03671
Ha = 213
613 n
mi
Hp = 206
345
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1668628
37 X = -581560
11
Y = 13962922
96 feet Y = 4249802
66 meter
Z = 17161391
49 Z = 5228144
88
XDOT = -23931
440073 XDOT = -7274
808320
YDOT = -7054
902866 feet/sec YDOT = -2231
794898 meter/sec
ZDOT = 3439
727441 ZDOT = 1013
040943
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13658362
55 X = 4163068
91
Y = -3402261
47 feet Y = -1037009
30 meter
Z = 17150354
09 Z = 5227427
93
XDOT = 1844
317240 XDOT = 562
147895
YDOT = 23885
226771 feet/sec YDOT = 7280
217120 meter/sec
ZDOT = 3296
116035 ZDOT = 1004
656167
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 11195
54977839
00016717 00000-0 10270-3 0 9062
2 25544 51
6370 22
9430 0011587 326
4714 33
5707 15
59805646 5181
Satellite: ISS
Catalog Number: 25544
Epoch time: 11195
54977839 = yrday
fracday
Element set: 906
Inclination: 51
6370 deg
RA of node: 22
9430 deg
Eccentricity:
0011587
Arg of perigee: 326
4714 deg
Mean anomaly: 33
5707 deg
Mean motion: 15
59805646 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 518
Checksum: 327
Coasting Arc #8 (Orbit 532)
---------------------------------------
Vector Time (GMT): 2011/196/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4237916
70 A = 6763592
14 meter
Y = -2497019
87 meter E =
0007517
Z = -4642613
94 I = 51
73232
XDOT = 5694
598730 Wp = 31
36364
YDOT = 4232
765509 meter/sec RA = 17
61240 deg
ZDOT = 2930
016730 TA = 267
68067
MA = 267
76674
Ha = 213
689 n
mi
Hp = 206
132
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13903926
17 X = 4288076
32
Y = -8192322
40 feet Y = -2449347
77 meter
Z = -15231673
04 Z = -4621905
17
XDOT = 18683
066698 XDOT = 5632
610744
YDOT = 13887
025949 feet/sec YDOT = 4296
098956 meter/sec
ZDOT = 9612
915780 ZDOT = 2957
530481
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12874480
25 X = -3924141
58
Y = -9861123
82 feet Y = -3005670
54 meter
Z = -15147381
56 Z = -4616921
90
XDOT = 5099
934545 XDOT = 1554
460049
YDOT = -21553
167942 feet/sec YDOT = -6569
405589 meter/sec
ZDOT = 9724
403832 ZDOT = 2963
998288
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 11196
51076332
00016717 00000-0 10270-3 0 9079
2 25544 51
6365 18
1093 0011494 329
7033 30
3457 15
59865385 5334
Satellite: ISS
Catalog Number: 25544
Epoch time: 11196
51076332 = yrday
fracday
Element set: 907
Inclination: 51
6365 deg
RA of node: 18
1093 deg
Eccentricity:
0011494
Arg of perigee: 329
7033 deg
Mean anomaly: 30
3457 deg
Mean motion: 15
59865385 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 533
Checksum: 307
Coasting Arc #9 (Orbit 548)
---------------------------------------
Vector Time (GMT): 2011/197/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6484884
21 A = 6771006
32 meter
Y = 125992
31 meter E =
0009086
Z = 1948161
87 I = 51
72887
XDOT = -1785
657230 Wp = 55
69319
YDOT = -4927
262871 meter/sec RA = 12
59437 deg
ZDOT = -5601
662881 TA = 102
81250
MA = 102
71096
Ha = 213
787 n
mi
Hp = 205
808
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21275866
84 X = -6495274
69
Y = 413360
59 feet Y = 53416
05 meter
Z = 6391607
18 Z = 1916633
87
XDOT = -5858
455479 XDOT = -1703
215733
YDOT = -16165
560599 feet/sec YDOT = -4946
769525 meter/sec
ZDOT = -18378
159059 ZDOT = -5610
137753
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8773306
46 X = 2674103
81
Y = 19428932
04 feet Y = 5921938
49 meter
Z = 6263522
40 Z = 1909121
63
XDOT = -11180
096296 XDOT = -3407
693351
YDOT = 11009
743621 feet/sec YDOT = 3355
769856 meter/sec
ZDOT = -18412
261135 ZDOT = -5612
057194
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 11197
53580565
00016717 00000-0 10270-3 0 9081
2 25544 51
6368 12
9543 0011800 333
1626 26
8918 15
59914096 5490
Satellite: ISS
Catalog Number: 25544
Epoch time: 11197
53580565 = yrday
fracday
Element set: 908
Inclination: 51
6368 deg
RA of node: 12
9543 deg
Eccentricity:
0011800
Arg of perigee: 333
1626 deg
Mean anomaly: 26
8918 deg
Mean motion: 15
59914096 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 549
Checksum: 325
Coasting Arc #10 (Orbit 564)
---------------------------------------
Vector Time (GMT): 2011/198/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6213253
73 A = 6771494
13 meter
Y = 2115176
14 meter E =
0018648
Z = 1614087
20 I = 51
70050
XDOT = -2920
440811 Wp = 25
29881
YDOT = 4188
106519 meter/sec RA = 7
60130 deg
ZDOT = 5745
721798 TA = 352
41704
MA = 352
44520
Ha = 213
868 n
mi
Hp = 205
574
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20384690
72 X = 6181298
89
Y = 6939554
27 feet Y = 2184477
69 meter
Z = 5295561
67 Z = 1644193
04
XDOT = -9581
498725 XDOT = -2994
966963
YDOT = 13740
506951 feet/sec YDOT = 4155
031089 meter/sec
ZDOT = 18850
793300 ZDOT = 5731
354052
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2003921
63 X = -610795
31
Y = -21409544
80 feet Y = -6525629
26 meter
Z = 5417720
18 Z = 1651321
11
XDOT = 14945
342605 XDOT = 4555
340426
YDOT = 3362
924898 feet/sec YDOT = 1025
019509 meter/sec
ZDOT = 18792
153734 ZDOT = 5727
848458
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 11198
56084350
00016717 00000-0 10270-3 0 9097
2 25544 51
6367 7
7984 0011502 337
5201 22
5449 15
59883326 5657
Satellite: ISS
Catalog Number: 25544
Epoch time: 11198
56084350 = yrday
fracday
Element set: 909
Inclination: 51
6367 deg
RA of node: 7
7984 deg
Eccentricity:
0011502
Arg of perigee: 337
5201 deg
Mean anomaly: 22
5449 deg
Mean motion: 15
59883326 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 565
Checksum: 318
Coasting Arc #11 (Orbit 579)
---------------------------------------
Vector Time (GMT): 2011/199/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3525123
34 A = 6764027
36 meter
Y = -3687219
29 meter E =
0015226
Z = -4454345
54 I = 51
64664
XDOT = 6544
689837 Wp = 19
97195
YDOT = -2294
347163 meter/sec RA = 2
58358 deg
ZDOT = -3269
481828 TA = 217
03491
MA = 217
14009
Ha = 214
045 n
mi
Hp = 205
179
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11565365
30 X = -3461992
23
Y = -12097176
16 feet Y = -3726286
02 meter
Z = -14613994
56 Z = -4471317
17
XDOT = 21472
079518 XDOT = 6585
741448
YDOT = -7527
385705 feet/sec YDOT = -2220
930655 meter/sec
ZDOT = -10726
646416 ZDOT = -3237
588918
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6070207
82 X = -1850199
34
Y = 15531877
26 feet Y = 4734116
19 meter
Z = -14682695
54 Z = -4475285
60
XDOT = -14837
524161 XDOT = -4522
477364
YDOT = -15849
452569 feet/sec YDOT = -4830
913143 meter/sec
ZDOT = -10596
944968 ZDOT = -3229
948826
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 11199
52180713
00016717 00000-0 10270-3 0 9106
2 25544 51
6376 2
9664 0011513 341
9440 18
1305 15
59916035 5808
Satellite: ISS
Catalog Number: 25544
Epoch time: 11199
52180713 = yrday
fracday
Element set: 910
Inclination: 51
6376 deg
RA of node: 2
9664 deg
Eccentricity:
0011513
Arg of perigee: 341
9440 deg
Mean anomaly: 18
1305 deg
Mean motion: 15
59916035 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 580
Checksum: 288
Coasting Arc #12 (Orbit 595)
---------------------------------------
Vector Time (GMT): 2011/200/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -600898
22 A = 6760877
05 meter
Y = 4201447
23 meter E =
0012563
Z = 5264110
29 I = 51
60478
XDOT = -7643
166006 Wp = 359
24691
YDOT = -215
429743 meter/sec RA = 357
52417 deg
ZDOT = -688
238743 TA = 97
39260
MA = 97
24982
Ha = 214
305 n
mi
Hp = 205
104
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1971450
85 X = -673406
55
Y = 13784275
69 feet Y = 4194321
84 meter
Z = 17270703
04 Z = 5261015
35
XDOT = -25076
003956 XDOT = -7636
845698
YDOT = -706
790497 feet/sec YDOT = -300
864895 meter/sec
ZDOT = -2258
001124 ZDOT = -725
353182
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13288971
48 X = 4050478
51
Y = -4211834
11 feet Y = -1283767
04 meter
Z = 17257860
50 Z = 5260195
88
XDOT = 10102
474634 XDOT = 3079
234268
YDOT = 21839
770153 feet/sec YDOT = 6656
761943 meter/sec
ZDOT = -2408
743607 ZDOT = -734
185051
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 11200
54682859
00016717 00000-0 10270-3 0 9110
2 25544 51
6371 357
8102 0011461 345
8935 14
1899 15
59865967 5964
Satellite: ISS
Catalog Number: 25544
Epoch time: 11200
54682859 = yrday
fracday
Element set: 911
Inclination: 51
6371 deg
RA of node: 357
8102 deg
Eccentricity:
0011461
Arg of perigee: 345
8935 deg
Mean anomaly: 14
1899 deg
Mean motion: 15
59865967 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 596
Checksum: 338
Coasting Arc #13 (Orbit 610)
---------------------------------------
Vector Time (GMT): 2011/201/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4425792
99 A = 6766784
45 meter
Y = -3537720
21 meter E =
0010787
Z = -3693192
30 I = 51
59632
XDOT = 5748
000271 Wp = 17
73247
YDOT = 2694
905479 meter/sec RA = 352
47404 deg
ZDOT = 4320
120091 TA = 298
09562
MA = 298
20463
Ha = 214
370 n
mi
Hp = 204
863
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14520318
21 X = 4482964
10
Y = -11606693
60 feet Y = -3487908
40 meter
Z = -12116772
64 Z = -3671553
50
XDOT = 18858
268606 XDOT = 5696
452087
YDOT = 8841
553408 feet/sec YDOT = 2758
894622 meter/sec
ZDOT = 14173
622346 ZDOT = 4347
918391
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16985058
60 X = -5177045
86
Y = -7693531
18 feet Y = -2344988
30 meter
Z = -12028654
08 Z = -3666333
76
XDOT = -1253
115974 XDOT = -381
949749
YDOT = -19500
761916 feet/sec YDOT = -5943
832232 meter/sec
ZDOT = 14286
358775 ZDOT = 4354
482155
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 11201
50777571
00016717 00000-0 10270-3 0 9124
2 25544 51
6386 352
9779 0011453 349
1127 10
9779 15
59923570 6111
Satellite: ISS
Catalog Number: 25544
Epoch time: 11201
50777571 = yrday
fracday
Element set: 912
Inclination: 51
6386 deg
RA of node: 352
9779 deg
Eccentricity:
0011453
Arg of perigee: 349
1127 deg
Mean anomaly: 10
9779 deg
Mean motion: 15
59923570 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 611
Checksum: 319
Coasting Arc #14 (Orbit 626)
---------------------------------------
Vector Time (GMT): 2011/202/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6521974
76 A = 6772365
89 meter
Y = 1784207
82 meter E =
0008736
Z = 410926
04 I = 51
58493
XDOT = -1617
245087 Wp = 68
48087
YDOT = -4507
501242 meter/sec RA = 347
46242 deg
ZDOT = -5991
140700 TA = 107
07882
MA = 106
98311
Ha = 214
439 n
mi
Hp = 204
555
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21397555
00 X = -6543437
57
Y = 5853700
18 feet Y = 1711155
09 meter
Z = 1348182
55 Z = 379190
68
XDOT = -5305
922203 XDOT = -1537
617633
YDOT = -14788
389902 feet/sec YDOT = -4525
140643 meter/sec
ZDOT = -19655
973426 ZDOT = -5998
804063
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15251007
93 X = 4648507
22
Y = 16120146
91 feet Y = 4913420
78 meter
Z = 1219173
02 Z = 371603
94
XDOT = -9423
503310 XDOT = -2872
283809
YDOT = 10433
321287 feet/sec YDOT = 3180
076328 meter/sec
ZDOT = -19686
809655 ZDOT = -6000
539583
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 11202
53277845
00016717 00000-0 10270-3 0 9138
2 25544 51
6378 347
8225 0011640 352
6142 7
4841 15
59959454 6273
Satellite: ISS
Catalog Number: 25544
Epoch time: 11202
53277845 = yrday
fracday
Element set: 913
Inclination: 51
6378 deg
RA of node: 347
8225 deg
Eccentricity:
0011640
Arg of perigee: 352
6142 deg
Mean anomaly: 7
4841 deg
Mean motion: 15
59959454 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 627
Checksum: 315
Coasting Arc #15 (Orbit 642)
---------------------------------------
Vector Time (GMT): 2011/203/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 899120
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6003168
39 A = 6768354
67 meter
Y = 630561
83 meter E =
0017647
Z = 3035653
14 I = 51
54382
XDOT = -3026
858658 Wp = 43
46459
YDOT = 5063
039396 meter/sec RA = 342
45534 deg
ZDOT = 4929
658285 TA = 351
54725
MA = 351
57694
Ha = 214
384 n
mi
Hp = 204
324
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19695434
34 X = 5980924
65
Y = 2068772
41 feet Y = 697568
32 meter
Z = 9959491
94 Z = 3064762
26
XDOT = -9930
638642 XDOT = -3107
196727
YDOT = 16611
021642 feet/sec YDOT = 5028
741656 meter/sec
ZDOT = 16173
419571 ZDOT = 4914
759193
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7742408
43 X = -2359886
09
Y = -18162516
36 feet Y = -5535934
99 meter
Z = 10077675
53 Z = 3071675
50
XDOT = 18067
395261 XDOT = 5506
942076
YDOT = 1246
358968 feet/sec YDOT = 379
890213 meter/sec
ZDOT = 16112
583899 ZDOT = 4911
115572
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 11203
55777349
00016717 00000-0 10270-3 0 9146
2 25544 51
6391 342
6677 0011473 356
3971 3
7101 15
59973606 6438
Satellite: ISS
Catalog Number: 25544
Epoch time: 11203
55777349 = yrday
fracday
Element set: 914
Inclination: 51
6391 deg
RA of node: 342
6677 deg
Eccentricity:
0011473
Arg of perigee: 356
3971 deg
Mean anomaly: 3
7101 deg
Mean motion: 15
59973606 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 643
Checksum: 318
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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