[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
July 23rd 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 11840 3 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 104 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 169 ET - UTC (sec) : 66 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
There are no maneuvers
Coasting Arc #1 (Orbit 642)
---------------------------------------
Vector Time (GMT): 2011/203/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5844878
10 A = 6767207
33 meter
Y = 879279
90 meter E =
0015808
Z = 3273386
08 I = 51
54201
XDOT = -3403
545048 Wp = 42
32340
YDOT = 5014
439640 meter/sec RA = 342
46029 deg
ZDOT = 4728
542522 TA = 355
89740
MA = 355
91034
Ha = 213
891 n
mi
Hp = 204
402
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19176109
25 X = 5818710
06
Y = 2884776
58 feet Y = 944494
33 meter
Z = 10739455
65 Z = 3301716
72
XDOT = -11166
486379 XDOT = -3482
334695
YDOT = 16451
573623 feet/sec YDOT = 4975
938236 meter/sec
ZDOT = 15513
590952 ZDOT = 4711
817264
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6774526
30 X = -2064875
62
Y = -18101587
41 feet Y = -5517363
84 meter
Z = 10854461
58 Z = 3308439
89
XDOT = 18531
659914 XDOT = 5648
449942
YDOT = 2329
672802 feet/sec YDOT = 710
084270 meter/sec
ZDOT = 15445
341585 ZDOT = 4707
740115
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
55719685
00016717 00000-0 10270-3 0 9000
2 25544 51
6396 342
6749 0011422 350
6059 9
4881 15
60146054 6430
Satellite: ISS
Catalog Number: 25544
Epoch time: 11203
55719685 = yrday
fracday
Element set: 900
Inclination: 51
6396 deg
RA of node: 342
6749 deg
Eccentricity:
0011422
Arg of perigee: 350
6059 deg
Mean anomaly: 9
4881 deg
Mean motion: 15
60146054 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 643
Checksum: 304
Coasting Arc #2 (Orbit 657)
---------------------------------------
Vector Time (GMT): 2011/204/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2850577
49 A = 6760334
93 meter
Y = -3285611
66 meter E =
0018891
Z = -5188616
75 I = 51
49072
XDOT = 6564
760517 Wp = 42
87276
YDOT = -3771
922088 meter/sec RA = 337
40794 deg
ZDOT = -1207
125803 TA = 215
45670
MA = 215
58242
Ha = 214
163 n
mi
Hp = 204
031
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9352288
36 X = -2788420
14
Y = -10779565
83 feet Y = -3317140
57 meter
Z = -17023020
83 Z = -5202314
04
XDOT = 21537
928207 XDOT = 6612
314921
YDOT = -12375
072468 feet/sec YDOT = -3698
244942 meter/sec
ZDOT = -3960
386493 ZDOT = -1175
119284
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4690328
96 X = -1429612
27
Y = 13408031
40 feet Y = 4086767
97 meter
Z = -17078439
14 Z = -5205508
25
XDOT = -20539
691601 XDOT = -6260
498000
YDOT = -12109
479180 feet/sec YDOT = -3690
969254 meter/sec
ZDOT = -3830
156908 ZDOT = -1167
431826
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 11204
51801493
00016717 00000-0 10270-3 0 9017
2 25544 51
6399 337
8428 0011583 354
6962 5
4069 15
60151366 6580
Satellite: ISS
Catalog Number: 25544
Epoch time: 11204
51801493 = yrday
fracday
Element set: 901
Inclination: 51
6399 deg
RA of node: 337
8428 deg
Eccentricity:
0011583
Arg of perigee: 354
6962 deg
Mean anomaly: 5
4069 deg
Mean motion: 15
60151366 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 658
Checksum: 311
Coasting Arc #3 (Orbit 673)
---------------------------------------
Vector Time (GMT): 2011/205/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1183933
86 A = 6762827
24 meter
Y = 4784601
39 meter E =
0016717
Z = 4631518
39 I = 51
47123
XDOT = -7027
025955 Wp = 25
35415
YDOT = 1081
411156 meter/sec RA = 332
33435 deg
ZDOT = -2894
735111 TA = 93
55974
MA = 93
36853
Ha = 214
385 n
mi
Hp = 203
940
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3884297
44 X = -1259847
10
Y = 15697511
13 feet Y = 4770937
00 meter
Z = 15195270
30 Z = 4625582
97
XDOT = -23054
547095 XDOT = -7024
534255
YDOT = 3547
936862 feet/sec YDOT = 1002
844895 meter/sec
ZDOT = -9497
162437 ZDOT = -2928
865964
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15497498
15 X = 4723637
44
Y = -4697707
32 feet Y = -1431861
19 meter
Z = 15170858
87 Z = 4624077
78
XDOT = 14565
936191 XDOT = 4439
697351
YDOT = 16735
605058 feet/sec YDOT = 5101
012422 meter/sec
ZDOT = -9635
845255 ZDOT = -2937
005634
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 11205
54287759
00016717 00000-0 10270-3 0 9025
2 25544 51
6400 332
6859 0011529 358
8613 1
2514 15
60123312 6740
Satellite: ISS
Catalog Number: 25544
Epoch time: 11205
54287759 = yrday
fracday
Element set: 902
Inclination: 51
6400 deg
RA of node: 332
6859 deg
Eccentricity:
0011529
Arg of perigee: 358
8613 deg
Mean anomaly: 1
2514 deg
Mean motion: 15
60123312 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 674
Checksum: 289
Coasting Arc #4 (Orbit 688)
---------------------------------------
Vector Time (GMT): 2011/206/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4492862
08 A = 6770360
44 meter
Y = -4681311
92 meter E =
0017959
Z = -1898615
58 I = 51
47134
XDOT = 4729
479546 Wp = 15
34750
YDOT = 2274
486693 meter/sec RA = 327
29663 deg
ZDOT = 5612
816580 TA = 323
61430
MA = 323
73625
Ha = 214
498 n
mi
Hp = 203
662
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14740361
16 X = 4554098
54
Y = -15358634
92 feet Y = -4630727
39 meter
Z = -6229053
74 Z = -1876641
26
XDOT = 15516
665178 XDOT = 4676
428501
YDOT = 7462
226684 feet/sec YDOT = 2327
077344 meter/sec
ZDOT = 18414
752560 ZDOT = 5635
663579
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20860669
92 X = -6358332
19
Y = -4371026
29 feet Y = -1332288
81 meter
Z = -6139511
68 Z = -1871323
16
XDOT = -2171
370557 XDOT = -661
833746
YDOT = -15496
422731 feet/sec YDOT = -4723
309648 meter/sec
ZDOT = 18507
394655 ZDOT = 5641
053891
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 11206
50367409
00016717 00000-0 10270-3 0 9034
2 25544 51
6408 327
8526 0011734 1
8625 358
2573 15
60158005 6894
Satellite: ISS
Catalog Number: 25544
Epoch time: 11206
50367409 = yrday
fracday
Element set: 903
Inclination: 51
6408 deg
RA of node: 327
8526 deg
Eccentricity:
0011734
Arg of perigee: 1
8625 deg
Mean anomaly: 358
2573 deg
Mean motion: 15
60158005 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 689
Checksum: 302
Coasting Arc #5 (Orbit 704)
---------------------------------------
Vector Time (GMT): 2011/207/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5915405
16 A = 6770337
56 meter
Y = 2786670
19 meter E =
0008238
Z = -1774491
78 I = 51
44697
XDOT = -725
355693 Wp = 43
76581
YDOT = -5131
527129 meter/sec RA = 322
28540 deg
ZDOT = -5650
438188 TA = 155
80055
MA = 155
76184
Ha = 214
531 n
mi
Hp = 203
339
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19407497
24 X = -5937506
55
Y = 9142618
73 feet Y = 2720397
17 meter
Z = -5821823
41 Z = -1803281
80
XDOT = -2379
775895 XDOT = -640
471582
YDOT = -16835
718928 feet/sec YDOT = -5139
163172 meter/sec
ZDOT = -18538
183031 ZDOT = -5653
756390
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18227296
57 X = 5555680
00
Y = 11252860
80 feet Y = 3429871
97 meter
Z = -5938925
64 Z = -1810184
53
XDOT = -12055
528459 XDOT = -3674
525074
YDOT = 9753
400980 feet/sec YDOT = 2972
836619 meter/sec
ZDOT = -18551
333812 ZDOT = -5654
446546
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 11207
52851473
00016717 00000-0 10270-3 0 9047
2 25544 51
6407 322
6965 0011721 5
8242 354
3049 15
60197834 7055
Satellite: ISS
Catalog Number: 25544
Epoch time: 11207
52851473 = yrday
fracday
Element set: 904
Inclination: 51
6407 deg
RA of node: 322
6965 deg
Eccentricity:
0011721
Arg of perigee: 5
8242 deg
Mean anomaly: 354
3049 deg
Mean motion: 15
60197834 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 705
Checksum: 296
Coasting Arc #6 (Orbit 720)
---------------------------------------
Vector Time (GMT): 2011/208/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4955398
46 A = 6762554
94 meter
Y = 390385
81 meter E =
0012448
Z = 4572961
15 I = 51
39882
XDOT = -3262
273834 Wp = 49
31551
YDOT = 6279
682573 meter/sec RA = 317
24483 deg
ZDOT = 3001
638010 TA = 10
71980
MA = 10
69329
Ha = 214
455 n
mi
Hp = 203
138
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16257868
98 X = 4928450
54
Y = 1280793
33 feet Y = 445648
82 meter
Z = 15003153
37 Z = 4596968
68
XDOT = -10702
998144 XDOT = -3346
833181
YDOT = 20602
633113 feet/sec YDOT = 6242
728651 meter/sec
ZDOT = 9847
893735 ZDOT = 2985
585567
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7986043
81 X = -2434146
15
Y = -14115498
58 feet Y = -4302403
97 meter
Z = 15100634
10 Z = 4602673
28
XDOT = 22068
055683 XDOT = 6726
343372
YDOT = -2029
449906 feet/sec YDOT = -618
576331 meter/sec
ZDOT = 9782
304168 ZDOT = 2981
646310
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 11208
55334361
00016717 00000-0 10270-3 0 9054
2 25544 51
6416 317
5405 0011735 9
3830 350
7543 15
60234138 7210
Satellite: ISS
Catalog Number: 25544
Epoch time: 11208
55334361 = yrday
fracday
Element set: 905
Inclination: 51
6416 deg
RA of node: 317
5405 deg
Eccentricity:
0011735
Arg of perigee: 9
3830 deg
Mean anomaly: 350
7543 deg
Mean motion: 15
60234138 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 721
Checksum: 278
Coasting Arc #7 (Orbit 735)
---------------------------------------
Vector Time (GMT): 2011/209/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2263183
25 A = 6760030
22 meter
Y = -3694398
92 meter E =
0019312
Z = -5202167
60 I = 51
36884
XDOT = 5705
009862 Wp = 60
35116
YDOT = -5006
412248 meter/sec RA = 312
16656 deg
ZDOT = 1085
847796 TA = 220
02225
MA = 220
16472
Ha = 214
706 n
mi
Hp = 202
806
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7425141
91 X = -2196432
90
Y = -12120731
38 feet Y = -3719333
35 meter
Z = -17067479
01 Z = -5213000
25
XDOT = 18717
223958 XDOT = 5755
293784
YDOT = -16425
237035 feet/sec YDOT = -4942
334336 meter/sec
ZDOT = 3562
492768 ZDOT = 1113
683679
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5725563
21 X = -1745151
67
Y = 12952481
02 feet Y = 3947916
22 meter
Z = -17111249
60 Z = -5215508
88
XDOT = -23235
170893 XDOT = -7082
080088
YDOT = -5468
514772 feet/sec YDOT = -1666
803303 meter/sec
ZDOT = 3675
858629 ZDOT = 1120
401710
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 11209
51411320
00016717 00000-0 10270-3 0 9063
2 25544 51
6416 312
7080 0011906 13
1872 346
9593 15
60239111 7369
Satellite: ISS
Catalog Number: 25544
Epoch time: 11209
51411320 = yrday
fracday
Element set: 906
Inclination: 51
6416 deg
RA of node: 312
7080 deg
Eccentricity:
0011906
Arg of perigee: 13
1872 deg
Mean anomaly: 346
9593 deg
Mean motion: 15
60239111 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 736
Checksum: 276
Coasting Arc #8 (Orbit 751)
---------------------------------------
Vector Time (GMT): 2011/210/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1080585
34 A = 6767040
33 meter
Y = 5804957
16 meter E =
0019561
Z = 3303602
19 I = 51
37238
XDOT = -5879
743483 Wp = 55
64171
YDOT = 1582
803379 meter/sec RA = 307
10109 deg
ZDOT = -4673
801626 TA = 85
67594
MA = 85
45245
Ha = 214
897 n
mi
Hp = 202
702
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3545227
49 X = -1161465
09
Y = 19045135
05 feet Y = 5792420
82 meter
Z = 10838589
86 Z = 3298157
01
XDOT = -19290
496991 XDOT = -5874
301779
YDOT = 5192
924473 feet/sec YDOT = 1517
083439 meter/sec
ZDOT = -15333
994836 ZDOT = -4702
351332
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17529956
61 X = 5343130
78
Y = -8274835
24 feet Y = -2522169
78 meter
Z = 10816124
99 Z = 3296754
90
XDOT = 14882
034150 XDOT = 4536
044009
YDOT = 11200
399523 feet/sec YDOT = 3413
881775 meter/sec
ZDOT = -15450
051223 ZDOT = -4709
175613
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 11210
53892373
00016717 00000-0 10270-3 0 9079
2 25544 51
6414 307
5520 0011910 17
3763 342
7798 15
60221097 7521
Satellite: ISS
Catalog Number: 25544
Epoch time: 11210
53892373 = yrday
fracday
Element set: 907
Inclination: 51
6414 deg
RA of node: 307
5520 deg
Eccentricity:
0011910
Arg of perigee: 17
3763 deg
Mean anomaly: 342
7798 deg
Mean motion: 15
60221097 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 752
Checksum: 294
Coasting Arc #9 (Orbit 767)
---------------------------------------
Vector Time (GMT): 2011/211/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3688680
55 A = 6771649
36 meter
Y = -5660438
70 meter E =
0023928
Z = 149568
09 I = 51
37100
XDOT = 3944
005736 Wp = 33
68497
YDOT = 2740
407712 meter/sec RA = 302
07702 deg
ZDOT = 6003
127953 TA = 327
93850
MA = 328
08383
Ha = 214
988 n
mi
Hp = 202
465
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12101970
30 X = 3750975
97
Y = -18570993
12 feet Y = -5618841
33 meter
Z = 490708
95 Z = 167638
05
XDOT = 12939
651364 XDOT = 3883
907519
YDOT = 8990
838949 feet/sec YDOT = 2784
175454 meter/sec
ZDOT = 19695
301683 ZDOT = 6022
141672
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -22112969
99 X = -6740033
25
Y = 1509382
97 feet Y = 460059
93 meter
Z = 564435
40 Z = 172039
91
XDOT = -421
470441 XDOT = -128
464191
YDOT = -14038
227669 feet/sec YDOT = -4278
851793 meter/sec
ZDOT = 19772
373709 ZDOT = 6026
619507
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 11211
56372312
00016717 00000-0 10270-3 0 9080
2 25544 51
6418 302
3961 0012113 20
5849 339
5792 15
60230332 7681
Satellite: ISS
Catalog Number: 25544
Epoch time: 11211
56372312 = yrday
fracday
Element set: 908
Inclination: 51
6418 deg
RA of node: 302
3961 deg
Eccentricity:
0012113
Arg of perigee: 20
5849 deg
Mean anomaly: 339
5792 deg
Mean motion: 15
60230332 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 768
Checksum: 285
Coasting Arc #10 (Orbit 782)
---------------------------------------
Vector Time (GMT): 2011/212/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4819283
90 A = 6766043
07 meter
Y = 3149890
51 meter E =
0015539
Z = -3574124
04 I = 51
33641
XDOT = -789
984199 Wp = 40
95900
YDOT = -6215
868627 meter/sec RA = 297
04940 deg
ZDOT = -4412
266344 TA = 181
53161
MA = 181
53637
Ha = 215
031 n
mi
Hp = 202
185
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15811298
88 X = -4836786
43
Y = 10334286
45 feet Y = 3095900
68 meter
Z = -11726128
75 Z = -3597577
82
XDOT = -2591
811677 XDOT = -698
985030
YDOT = -20393
269774 feet/sec YDOT = -6224
193654 meter/sec
ZDOT = -14475
939449 ZDOT = -4415
883309
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17831146
64 X = 5434933
49
Y = 6049575
41 feet Y = 1843910
58 meter
Z = -11821573
12 Z = -3603215
49
XDOT = -14094
035200 XDOT = -4295
861929
YDOT = 13222
682448 feet/sec YDOT = 4030
273610 meter/sec
ZDOT = -14490
283092 ZDOT = -4416
638286
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 11212
52446247
00016717 00000-0 10270-3 0 9097
2 25544 51
6408 297
5628 0012003 24
1632 336
0084 15
60256573 7831
Satellite: ISS
Catalog Number: 25544
Epoch time: 11212
52446247 = yrday
fracday
Element set: 909
Inclination: 51
6408 deg
RA of node: 297
5628 deg
Eccentricity:
0012003
Arg of perigee: 24
1632 deg
Mean anomaly: 336
0084 deg
Mean motion: 15
60256573 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 783
Checksum: 292
Coasting Arc #11 (Orbit 798)
---------------------------------------
Vector Time (GMT): 2011/213/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4182157
97 A = 6759552
88 meter
Y = 842931
83 meter E =
0012462
Z = 5235088
68 I = 51
30245
XDOT = -2335
986084 Wp = 41
16526
YDOT = 7289
009187 meter/sec RA = 291
97575 deg
ZDOT = 700
793021 TA = 42
17384
MA = 42
07803
Ha = 214
921 n
mi
Hp = 202
039
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13720990
70 X = 4146990
84
Y = 2765524
39 feet Y = 889502
47 meter
Z = 17175487
80 Z = 5255319
70
XDOT = -7663
996339 XDOT = -2420
723826
YDOT = 23914
072137 feet/sec YDOT = 7262
412949 meter/sec
ZDOT = 2299
189703 ZDOT = 689
239510
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6411198
15 X = -1954133
20
Y = -12328105
42 feet Y = -3757606
53 meter
Z = 17257619
97 Z = 5260122
57
XDOT = 22523
911884 XDOT = 6865
288342
YDOT = -8599
086732 feet/sec YDOT = -2621
001636 meter/sec
ZDOT = 2251
865936 ZDOT = 686
368737
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 11213
54924035
00016717 00000-0 10270-3 0 9108
2 25544 51
6409 292
4062 0012055 27
5142 332
6650 15
60309709 7996
Satellite: ISS
Catalog Number: 25544
Epoch time: 11213
54924035 = yrday
fracday
Element set: 910
Inclination: 51
6409 deg
RA of node: 292
4062 deg
Eccentricity:
0012055
Arg of perigee: 27
5142 deg
Mean anomaly: 332
6650 deg
Mean motion: 15
60309709 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 799
Checksum: 288
Coasting Arc #12 (Orbit 813)
---------------------------------------
Vector Time (GMT): 2011/214/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2265745
38 A = 6763129
86 meter
Y = -4630782
51 meter E =
0016573
Z = -4386132
76 I = 51
30297
XDOT = 4411
895878 Wp = 64
02043
YDOT = -5309
748295 meter/sec RA = 286
89252 deg
ZDOT = 3343
840028 TA = 239
85267
MA = 240
01700
Ha = 215
139 n
mi
Hp = 201
731
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7433547
82 X = -2192488
08
Y = -15192855
99 feet Y = -4655709
77 meter
Z = -14390199
34 Z = -4396961
66
XDOT = 14474
724008 XDOT = 4454
699185
YDOT = -17420
434038 feet/sec YDOT = -5260
172519 meter/sec
ZDOT = 10970
603766 ZDOT = 3365
376436
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6931138
71 X = -2112611
08
Y = 15387622
61 feet Y = 4690147
37 meter
Z = -14433943
67 Z = -4399466
03
XDOT = -21484
040559 XDOT = -6548
335563
YDOT = 643
719535 feet/sec YDOT = 196
205714 meter/sec
ZDOT = 11058
361075 ZDOT = 3370
588456
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 11214
50996279
00016717 00000-0 10270-3 0 9115
2 25544 51
6397 287
5731 0012240 31
6555 328
5334 15
60318847 8144
Satellite: ISS
Catalog Number: 25544
Epoch time: 11214
50996279 = yrday
fracday
Element set: 911
Inclination: 51
6397 deg
RA of node: 287
5731 deg
Eccentricity:
0012240
Arg of perigee: 31
6555 deg
Mean anomaly: 328
5334 deg
Mean motion: 15
60318847 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 814
Checksum: 313
Coasting Arc #13 (Orbit 829)
---------------------------------------
Vector Time (GMT): 2011/215/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -281578
39 A = 6770595
09 meter
Y = 6626378
03 meter E =
0019362
Z = 1355132
59 I = 51
31999
XDOT = -4941
660655 Wp = 80
33281
YDOT = 988
714602 meter/sec RA = 281
84772 deg
ZDOT = -5787
557585 TA = 84
80857
MA = 84
58764
Ha = 215
292 n
mi
Hp = 201
590
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -923813
63 X = -362237
79
Y = 21740085
39 feet Y = 6622778
24 meter
Z = 4445973
08 Z = 1353568
88
XDOT = -16212
797425 XDOT = -4924
234928
YDOT = 3243
814310 feet/sec YDOT = 933
551451 meter/sec
ZDOT = -18988
049818 ZDOT = -5811
521440
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17047504
98 X = 5196079
52
Y = -13525041
67 feet Y = -4122432
70 meter
Z = 4439284
06 Z = 1353093
78
XDOT = 12010
508493 XDOT = 3660
802989
YDOT = 8794
462468 feet/sec YDOT = 2680
552160 meter/sec
ZDOT = -19085
439435 ZDOT = -5817
241940
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 11215
53472241
00016717 00000-0 10270-3 0 9128
2 25544 51
6394 282
4158 0012383 35
0035 325
1933 15
60325011 8304
Satellite: ISS
Catalog Number: 25544
Epoch time: 11215
53472241 = yrday
fracday
Element set: 912
Inclination: 51
6394 deg
RA of node: 282
4158 deg
Eccentricity:
0012383
Arg of perigee: 35
0035 deg
Mean anomaly: 325
1933 deg
Mean motion: 15
60325011 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 830
Checksum: 266
Coasting Arc #14 (Orbit 845)
---------------------------------------
Vector Time (GMT): 2011/216/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2543289
69 A = 6769145
46 meter
Y = -5823684
94 meter E =
0025176
Z = 2289041
12 I = 51
30957
XDOT = 3899
342845 Wp = 56
59368
YDOT = 3838
424748 meter/sec RA = 276
82459 deg
ZDOT = 5403
870421 TA = 329
13931
MA = 329
28706
Ha = 215
335 n
mi
Hp = 201
438
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8344126
29 X = 2597102
63
Y = -19106577
88 feet Y = -5794943
49 meter
Z = 7509977
43 Z = 2301526
86
XDOT = 12793
119570 XDOT = 3829
880316
YDOT = 12593
257046 feet/sec YDOT = 3881
641075 meter/sec
ZDOT = 17729
233665 ZDOT = 5422
644560
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19761244
10 X = -6023227
20
Y = 6588647
00 feet Y = 2008219
61 meter
Z = 7560984
42 Z = 2304588
05
XDOT = 1376
939901 XDOT = 419
691282
YDOT = -16412
483060 feet/sec YDOT = -5002
524837 meter/sec
ZDOT = 17805
301366 ZDOT = 5427
055856
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 11216
55947224
00016717 00000-0 10270-3 0 9130
2 25544 51
6391 277
2590 0012434 38
9795 321
2255 15
60313528 8466
Satellite: ISS
Catalog Number: 25544
Epoch time: 11216
55947224 = yrday
fracday
Element set: 913
Inclination: 51
6391 deg
RA of node: 277
2590 deg
Eccentricity:
0012434
Arg of perigee: 38
9795 deg
Mean anomaly: 321
2255 deg
Mean motion: 15
60313528 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 846
Checksum: 310
Coasting Arc #15 (Orbit 860)
---------------------------------------
Vector Time (GMT): 2011/217/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3977096
85 A = 6761247
66 meter
Y = 2546674
92 meter E =
0023557
Z = -4860482
14 I = 51
28037
XDOT = -1666
743475 Wp = 57
32641
YDOT = -7097
596553 meter/sec RA = 271
76621 deg
ZDOT = -2350
849588 TA = 189
48907
MA = 189
53365
Ha = 215
441 n
mi
Hp = 201
168
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13048218
01 X = -3981667
56
Y = 8355232
68 feet Y = 2502175
23 meter
Z = -15946463
71 Z = -4879813
70
XDOT = -5468
318487 XDOT = -1575
833000
YDOT = -23286
077929 feet/sec YDOT = -7115
726696 meter/sec
ZDOT = -7712
761114 ZDOT = -2358
726006
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14936851
82 X = 4552752
43
Y = 3800234
44 feet Y = 1158311
46 meter
Z = -16025114
26 Z = -4884454
83
XDOT = -13089
667037 XDOT = -3989
730513
YDOT = 18734
608180 feet/sec YDOT = 5710
308573 meter/sec
ZDOT = -7744
406018 ZDOT = -2360
494954
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 11217
52016586
00016717 00000-0 10270-3 0 9147
2 25544 51
6388 272
4241 0012412 42
3845 317
8267 15
60320079 8613
Satellite: ISS
Catalog Number: 25544
Epoch time: 11217
52016586 = yrday
fracday
Element set: 914
Inclination: 51
6388 deg
RA of node: 272
4241 deg
Eccentricity:
0012412
Arg of perigee: 42
3845 deg
Mean anomaly: 317
8267 deg
Mean motion: 15
60320079 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 861
Checksum: 294
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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