[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
April 16th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 11302 11 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 131 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
116/12:16:31
624 3
7 6
0 6
0
N/A -2
1 -0
1 214
2
000/00:13:01
249 -4
3 -0
1 212
7
Coasting Arc #1 (Orbit 793)
---------------------------------------
Vector Time (GMT): 2012/104/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925359
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4174300
51 A = 6765399
37 meter
Y = 87936
49 meter E =
0005608
Z = 5328149
20 I = 51
96670
XDOT = -445
243727 Wp = 278
14646
YDOT = -7655
349445 meter/sec RA = 85
37432 deg
ZDOT = -221
902840 TA = 173
96151
MA = 173
95475
Ha = 211
926 n
mi
Hp = 211
249
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13695211
63 X = -4200856
49
Y = 288505
55 feet Y = 41108
57 meter
Z = 17480804
47 Z = 5307806
17
XDOT = -1460
773384 XDOT = -358
529016
YDOT = -25115
975869 feet/sec YDOT = -7659
843594 meter/sec
ZDOT = -728
027689 ZDOT = -223
854940
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12755495
81 X = -3887875
12
Y = 5277855
68 feet Y = 1608690
41 meter
Z = 17397187
94 Z = 5302662
88
XDOT = -10086
071050 XDOT = -3074
234456
YDOT = -21945
489938 feet/sec YDOT = -6688
985333 meter/sec
ZDOT = -735
447352 ZDOT = -224
164353
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 12104
54772299
00016717 00000-0 10270-3 0 9000
2 25544 51
6392 85
9152 0007994 272
6563 87
3677 15
58248063 7948
Satellite: ISS
Catalog Number: 25544
Epoch time: 12104
54772299 = yrday
fracday
Element set: 900
Inclination: 51
6392 deg
RA of node: 85
9152 deg
Eccentricity:
0007994
Arg of perigee: 272
6563 deg
Mean anomaly: 87
3677 deg
Mean motion: 15
58248063 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 794
Checksum: 342
Coasting Arc #2 (Orbit 808)
---------------------------------------
Vector Time (GMT): 2012/105/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925359
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4003318
50 A = 6769405
07 meter
Y = 3316586
74 meter E =
0002080
Z = -4337111
47 I = 51
97683
XDOT = -1666
029989 Wp = 176
57875
YDOT = 6612
411222 meter/sec RA = 80
35920 deg
ZDOT = 3516
762432 TA = 129
01130
MA = 128
99278
Ha = 212
648 n
mi
Hp = 211
763
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13134247
04 X = 3987002
87
Y = 10881190
11 feet Y = 3361262
89 meter
Z = -14229368
33 Z = -4317703
37
XDOT = -5465
977655 XDOT = -1756
931083
YDOT = 21694
262539 feet/sec YDOT = 6593
272563 meter/sec
ZDOT = 11537
934487 ZDOT = 3508
447830
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16357059
56 X = 4985631
75
Y = 5060793
60 feet Y = 1542529
89 meter
Z = -14149863
50 Z = -4312878
40
XDOT = 3464
706261 XDOT = 1056
042468
YDOT = 20982
308675 feet/sec YDOT = 6395
407684 meter/sec
ZDOT = 11503
232208 ZDOT = 3506
185177
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 12105
50968418
00016717 00000-0 10270-3 0 9018
2 25544 51
6392 81
0894 0007971 276
6652 83
3595 15
58264341 8095
Satellite: ISS
Catalog Number: 25544
Epoch time: 12105
50968418 = yrday
fracday
Element set: 901
Inclination: 51
6392 deg
RA of node: 81
0894 deg
Eccentricity:
0007971
Arg of perigee: 276
6652 deg
Mean anomaly: 83
3595 deg
Mean motion: 15
58264341 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 809
Checksum: 327
Coasting Arc #3 (Orbit 824)
---------------------------------------
Vector Time (GMT): 2012/106/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925359
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3031131
46 A = 6775658
45 meter
Y = -5751761
66 meter E =
0006365
Z = 1894319
55 I = 51
99240
XDOT = 3585
392124 Wp = 129
15776
YDOT = -3753
859946 meter/sec RA = 75
37283 deg
ZDOT = -5652
140468 TA = 30
04751
MA = 30
01101
Ha = 212
717 n
mi
Hp = 211
542
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9944657
01 X = -2975790
97
Y = -18870609
11 feet Y = -5785348
09 meter
Z = 6214959
14 Z = 1879729
27
XDOT = 11763
097519 XDOT = 3654
558857
YDOT = -12315
813472 feet/sec YDOT = -3713
379518 meter/sec
ZDOT = -18543
767941 ZDOT = -5634
554567
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16620036
79 X = -5065787
21
Y = -13398005
37 feet Y = -4083712
04 meter
Z = 6155455
90 Z = 1876182
96
XDOT = 5072
827645 XDOT = 1546
197866
YDOT = -14792
299293 feet/sec YDOT = -4508
692825 meter/sec
ZDOT = -18471
182896 ZDOT = -5630
016547
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 12106
53575774
00016717 00000-0 10270-3 0 9022
2 25544 51
6394 75
9415 0008057 280
9799 79
0449 15
58324742 8254
Satellite: ISS
Catalog Number: 25544
Epoch time: 12106
53575774 = yrday
fracday
Element set: 902
Inclination: 51
6394 deg
RA of node: 75
9415 deg
Eccentricity:
0008057
Arg of perigee: 280
9799 deg
Mean anomaly: 79
0449 deg
Mean motion: 15
58324742 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 825
Checksum: 340
Coasting Arc #4 (Orbit 840)
---------------------------------------
Vector Time (GMT): 2012/107/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925359
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1338282
15 A = 6776414
25 meter
Y = 6529007
54 meter E =
0009889
Z = 1188058
16 I = 51
98684
XDOT = -4915
869218 Wp = 22
98655
YDOT = -66
676303 meter/sec RA = 70
40673 deg
ZDOT = 5896
286521 TA = 349
88372
MA = 349
90361
Ha = 212
829 n
mi
Hp = 211
319
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4390689
45 X = 1259402
67
Y = 21420628
41 feet Y = 6543532
09 meter
Z = 3897828
61 Z = 1194367
37
XDOT = -16128
179849 XDOT = -4943
401140
YDOT = -218
754274 feet/sec YDOT = -121
802067 meter/sec
ZDOT = 19344
772052 ZDOT = 5872
338552
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12774410
52 X = 3893640
33
Y = 17740836
71 feet Y = 5407407
03 meter
Z = 3923224
67 Z = 1195798
88
XDOT = -13609
626035 XDOT = -4148
214015
YDOT = 5538
077422 feet/sec YDOT = 1688
005998 meter/sec
ZDOT = 19246
347574 ZDOT = 5866
286740
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 12107
56181131
00016717 00000-0 10270-3 0 9037
2 25544 51
6395 70
7936 0007998 283
4293 76
5971 15
58372386 8413
Satellite: ISS
Catalog Number: 25544
Epoch time: 12107
56181131 = yrday
fracday
Element set: 903
Inclination: 51
6395 deg
RA of node: 70
7936 deg
Eccentricity:
0007998
Arg of perigee: 283
4293 deg
Mean anomaly: 76
5971 deg
Mean motion: 15
58372386 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 841
Checksum: 334
Coasting Arc #5 (Orbit 855)
---------------------------------------
Vector Time (GMT): 2012/108/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925359
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 827016
79 A = 6770599
56 meter
Y = -5489171
39 meter E =
0004511
Z = -3878512
11 I = 51
95717
XDOT = 5270
717403 Wp = 340
64063
YDOT = 3726
784802 meter/sec RA = 65
42579 deg
ZDOT = -4145
036555 TA = 246
01522
MA = 246
06245
Ha = 213
102 n
mi
Hp = 211
153
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2713309
69 X = 907177
39
Y = -18009092
48 feet Y = -5479475
30 meter
Z = -12724777
25 Z = -3874299
30
XDOT = 17292
379932 XDOT = 5248
787763
YDOT = 12226
984258 feet/sec YDOT = 3785
602260 meter/sec
ZDOT = -13599
201295 ZDOT = -4119
485101
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5148985
62 X = -1569410
82
Y = -17482259
53 feet Y = -5328592
70 meter
Z = -12707004
62 Z = -3873095
01
XDOT = 19653
212854 XDOT = 5990
299278
YDOT = 4033
287835 feet/sec YDOT = 1229
346132 meter/sec
ZDOT = -13494
493729 ZDOT = -4113
121689
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 12108
52372070
00016717 00000-0 10270-3 0 9049
2 25544 51
6403 65
9672 0008067 288
5418 71
4860 15
58382862 8566
Satellite: ISS
Catalog Number: 25544
Epoch time: 12108
52372070 = yrday
fracday
Element set: 904
Inclination: 51
6403 deg
RA of node: 65
9672 deg
Eccentricity:
0008067
Arg of perigee: 288
5418 deg
Mean anomaly: 71
4860 deg
Mean motion: 15
58382862 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 856
Checksum: 319
Coasting Arc #6 (Orbit 871)
---------------------------------------
Vector Time (GMT): 2012/109/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925359
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3036038
50 A = 6765179
21 meter
Y = 2992874
83 meter E =
0004766
Z = 5256697
39 I = 51
92634
XDOT = -4409
129361 Wp = 283
99964
YDOT = -6201
235866 meter/sec RA = 60
41301 deg
ZDOT = 985
992306 TA = 156
61593
MA = 156
59425
Ha = 213
308 n
mi
Hp = 210
898
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9960756
24 X = -3094815
87
Y = 9819143
15 feet Y = 2958595
76 meter
Z = 17246382
51 Z = 5241805
30
XDOT = -14465
647511 XDOT = -4344
247958
YDOT = -20345
262028 feet/sec YDOT = -6250
178626 meter/sec
ZDOT = 3234
882893 ZDOT = 964
730867
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4694577
79 X = -1430907
31
Y = 13255539
19 feet Y = 4040288
34 meter
Z = 17184922
66 Z = 5237964
43
XDOT = -21013
670235 XDOT = -6404
966688
YDOT = -11515
421286 feet/sec YDOT = -3509
900408 meter/sec
ZDOT = 3148
026076 ZDOT = 959
518348
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 12109
54973689
00016717 00000-0 10270-3 0 9056
2 25544 51
6410 60
8198 0008198 291
8493 68
1790 15
58422590 8722
Satellite: ISS
Catalog Number: 25544
Epoch time: 12109
54973689 = yrday
fracday
Element set: 905
Inclination: 51
6410 deg
RA of node: 60
8198 deg
Eccentricity:
0008198
Arg of perigee: 291
8493 deg
Mean anomaly: 68
1790 deg
Mean motion: 15
58422590 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 872
Checksum: 342
Coasting Arc #7 (Orbit 886)
---------------------------------------
Vector Time (GMT): 2012/110/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925359
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4723883
91 A = 6766967
93 meter
Y = 159286
04 meter E =
0003673
Z = -4845832
49 I = 51
91657
XDOT = 2343
421445 Wp = 90
37622
YDOT = 6860
380916 meter/sec RA = 55
38786 deg
ZDOT = 2511
567106 TA = 204
19068
MA = 204
20793
Ha = 213
541 n
mi
Hp = 210
770
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15498306
78 X = 4745291
91
Y = 522592
00 feet Y = 212230
78 meter
Z = -15898400
55 Z = -4822831
79
XDOT = 7688
390566 XDOT = 2254
332321
YDOT = 22507
811403 feet/sec YDOT = 6886
088562 meter/sec
ZDOT = 8240
049559 ZDOT = 2522
734589
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14109769
79 X = 4300657
83
Y = -6661932
47 feet Y = -2030557
02 meter
Z = -15803885
84 Z = -4817024
40
XDOT = 16593
387072 XDOT = 5057
664379
YDOT = 15501
852699 feet/sec YDOT = 4724
964703 meter/sec
ZDOT = 8285
351330 ZDOT = 2525
375085
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 12110
51161030
00016717 00000-0 10270-3 0 9065
2 25544 51
6412 55
9930 0008172 295
6988 64
3323 15
58427842 8877
Satellite: ISS
Catalog Number: 25544
Epoch time: 12110
51161030 = yrday
fracday
Element set: 906
Inclination: 51
6412 deg
RA of node: 55
9930 deg
Eccentricity:
0008172
Arg of perigee: 295
6988 deg
Mean anomaly: 64
3323 deg
Mean motion: 15
58427842 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 887
Checksum: 306
Coasting Arc #8 (Orbit 902)
---------------------------------------
Vector Time (GMT): 2012/111/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925359
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5360539
64 A = 6773565
29 meter
Y = -3080362
60 meter E =
0006317
Z = 2763949
87 I = 51
92181
XDOT = 577
027064 Wp = 76
56614
YDOT = -5646
593413 meter/sec RA = 50
38660 deg
ZDOT = -5162
586369 TA = 72
20380
MA = 72
13488
Ha = 213
555 n
mi
Hp = 210
474
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17587072
32 X = -5339122
85
Y = -10106176
51 feet Y = -3140187
56 meter
Z = 9068077
01 Z = 2737960
41
XDOT = 1893
133413 XDOT = 665
204607
YDOT = -18525
568940 feet/sec YDOT = -5639
648014 meter/sec
ZDOT = -16937
619322 ZDOT = -5159
568638
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20323056
66 X = -6194467
67
Y = -577998
85 feet Y = -176174
05 meter
Z = 8961541
28 Z = 2731477
78
XDOT = -7030
453817 XDOT = -2142
882323
YDOT = -15791
731423 feet/sec YDOT = -4813
319738 meter/sec
ZDOT = -16924
717524 ZDOT = -5158
653901
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 12111
53758912
00016717 00000-0 10270-3 0 9070
2 25544 51
6421 50
8453 0008179 299
7544 60
2797 15
58467986 9033
Satellite: ISS
Catalog Number: 25544
Epoch time: 12111
53758912 = yrday
fracday
Element set: 907
Inclination: 51
6421 deg
RA of node: 50
8453 deg
Eccentricity:
0008179
Arg of perigee: 299
7544 deg
Mean anomaly: 60
2797 deg
Mean motion: 15
58467986 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 903
Checksum: 337
Coasting Arc #9 (Orbit 918)
---------------------------------------
Vector Time (GMT): 2012/112/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925359
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4592828
24 A = 6776657
96 meter
Y = 4963373
41 meter E =
0013182
Z = 272306
24 I = 51
91220
XDOT = -3645
840435 Wp = 11
01819
YDOT = 3040
549856 meter/sec RA = 45
41198 deg
ZDOT = 6036
248110 TA = 351
91210
MA = 351
93333
Ha = 213
721 n
mi
Hp = 210
163
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15068334
12 X = 4535662
61
Y = 16284033
49 feet Y = 5014413
63 meter
Z = 893393
17 Z = 294479
32
XDOT = -11961
418751 XDOT = -3708
892762
YDOT = 9975
557271 feet/sec YDOT = 2999
427521 meter/sec
ZDOT = 19803
963616 ZDOT = 6018
383187
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21088232
39 X = 6427693
23
Y = 6880454
93 feet Y = 2097162
66 meter
Z = 984066
08 Z = 299943
34
XDOT = -5187
165205 XDOT = -1581
047954
YDOT = 13061
437867 feet/sec YDOT = 3981
126262 meter/sec
ZDOT = 19730
271420 ZDOT = 6013
786729
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 12112
56354843
00016717 00000-0 10270-3 0 9080
2 25544 51
6422 45
6970 0008221 303
3792 56
6575 15
58486520 9190
Satellite: ISS
Catalog Number: 25544
Epoch time: 12112
56354843 = yrday
fracday
Element set: 908
Inclination: 51
6422 deg
RA of node: 45
6970 deg
Eccentricity:
0008221
Arg of perigee: 303
3792 deg
Mean anomaly: 56
6575 deg
Mean motion: 15
58486520 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 919
Checksum: 314
Coasting Arc #10 (Orbit 933)
---------------------------------------
Vector Time (GMT): 2012/113/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925359
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2461804
01 A = 6772084
90 meter
Y = -5423500
05 meter E =
0004751
Z = -3225914
88 I = 51
87641
XDOT = 5980
070550 Wp = 334
93011
YDOT = 145
332290 meter/sec RA = 40
43267 deg
ZDOT = -4801
151404 TA = 242
32689
MA = 242
37511
Ha = 213
808 n
mi
Hp = 209
867
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8076784
81 X = -2385303
31
Y = -17793635
34 feet Y = -5450601
80 meter
Z = -10583710
23 Z = -3237688
48
XDOT = 19619
654036 XDOT = 6001
324297
YDOT = 476
811974 feet/sec YDOT = 212
323858 meter/sec
ZDOT = -15751
809069 ZDOT = -4772
048337
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15865193
02 X = -4835710
83
Y = -11363437
66 feet Y = -3463575
80 meter
Z = -10631592
94 Z = -3240509
53
XDOT = 16458
766546 XDOT = 5016
632043
YDOT = -8332
928082 feet/sec YDOT = -2539
876480 meter/sec
ZDOT = -15632
223793 ZDOT = -4764
701812
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 12113
52536693
00016717 00000-0 10270-3 0 9093
2 25544 51
6433 40
8709 0008212 307
2116 52
8289 15
58532172 9344
Satellite: ISS
Catalog Number: 25544
Epoch time: 12113
52536693 = yrday
fracday
Element set: 909
Inclination: 51
6433 deg
RA of node: 40
8709 deg
Eccentricity:
0008212
Arg of perigee: 307
2116 deg
Mean anomaly: 52
8289 deg
Mean motion: 15
58532172 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 934
Checksum: 301
Coasting Arc #11 (Orbit 949)
---------------------------------------
Vector Time (GMT): 2012/114/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925359
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -576780
83 A = 6765557
06 meter
Y = 4463328
21 meter E =
0002784
Z = 5052566
82 I = 51
83095
XDOT = -6800
632601 Wp = 319
52469
YDOT = -3014
353804 meter/sec RA = 35
42007 deg
ZDOT = 1889
130973 TA = 112
24482
MA = 112
21528
Ha = 213
914 n
mi
Hp = 209
662
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1892325
56 X = -651192
47
Y = 14643465
26 feet Y = 4456462
27 meter
Z = 16576662
79 Z = 5049584
02
XDOT = -22311
786749 XDOT = -6775
597177
YDOT = -9889
612218 feet/sec YDOT = -3090
262689 meter/sec
ZDOT = 6197
936262 ZDOT = 1856
154054
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5865464
87 X = 1787793
69
Y = 13565708
01 feet Y = 4134827
80 meter
Z = 16563985
28 Z = 5048702
71
XDOT = -23253
913003 XDOT = -7087
792683
YDOT = 2662
341751 feet/sec YDOT = 811
481766 meter/sec
ZDOT = 6062
703389 ZDOT = 1847
911993
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 12114
55128699
00016717 00000-0 10270-3 0 9102
2 25544 51
6432 35
7228 0008248 309
8823 50
1606 15
58575512 9501
Satellite: ISS
Catalog Number: 25544
Epoch time: 12114
55128699 = yrday
fracday
Element set: 910
Inclination: 51
6432 deg
RA of node: 35
7228 deg
Eccentricity:
0008248
Arg of perigee: 309
8823 deg
Mean anomaly: 50
1606 deg
Mean motion: 15
58575512 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 950
Checksum: 307
Coasting Arc #12 (Orbit 964)
---------------------------------------
Vector Time (GMT): 2012/115/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925359
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3663347
43 A = 6765393
10 meter
Y = -2511339
78 meter E =
0007636
Z = -5108695
43 I = 51
80533
XDOT = 5682
564906 Wp = 68
33084
YDOT = 4869
611734 meter/sec RA = 30
38588 deg
ZDOT = 1685
816164 TA = 217
88003
MA = 217
93378
Ha = 214
132 n
mi
Hp = 209
499
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12018856
39 X = 3715974
75
Y = -8239303
73 feet Y = -2470079
67 meter
Z = -16760811
78 Z = -5090770
95
XDOT = 18643
585649 XDOT = 5619
500130
YDOT = 15976
416451 feet/sec YDOT = 4932
805063 meter/sec
ZDOT = 5530
892928 ZDOT = 1713
269097
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5884425
10 X = 1793572
77
Y = -13423275
71 feet Y = -4091414
44 meter
Z = -16686912
73 Z = -5086171
00
XDOT = 23276
949475 XDOT = 7094
814200
YDOT = 3208
262588 feet/sec YDOT = 977
878437 meter/sec
ZDOT = 5643
242620 ZDOT = 1720
060351
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 12115
51307115
00016717 00000-0 10270-3 0 9112
2 25544 51
6437 30
8960 0008273 314
2378 45
8097 15
58580185 9651
Satellite: ISS
Catalog Number: 25544
Epoch time: 12115
51307115 = yrday
fracday
Element set: 911
Inclination: 51
6437 deg
RA of node: 30
8960 deg
Eccentricity:
0008273
Arg of perigee: 314
2378 deg
Mean anomaly: 45
8097 deg
Mean motion: 15
58580185 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 965
Checksum: 307
Coasting Arc #13 (Orbit 980)
---------------------------------------
Vector Time (GMT): 2012/116/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925359
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5885005
06 A = 6771696
40 meter
Y = 125227
89 meter E =
0009128
Z = 3347731
59 I = 51
79941
XDOT = -2787
058176 Wp = 50
69017
YDOT = -5400
180557 meter/sec RA = 25
36792 deg
ZDOT = -4683
223977 TA = 90
32697
MA = 90
22238
Ha = 214
208 n
mi
Hp = 209
260
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19307759
39 X = -5902230
74
Y = 410852
67 feet Y = 59321
76 meter
Z = 10983371
35 Z = 3319100
28
XDOT = -9143
891652 XDOT = -2703
714770
YDOT = -17717
127811 feet/sec YDOT = -5430
881093 meter/sec
ZDOT = -15364
908061 ZDOT = -4696
561203
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16004659
26 X = -4878220
14
Y = 10926125
82 feet Y = 3330283
15 meter
Z = 10865701
78 Z = 3311865
90
XDOT = -16461
375232 XDOT = -5017
427171
YDOT = -8732
089475 feet/sec YDOT = -2661
540872 meter/sec
ZDOT = -15419
193059 ZDOT = -4699
770044
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 12116
53895470
00016717 00000-0 10270-3 0 9122
2 25544 51
6433 25
7477 0008232 317
9099 42
1423 15
58597793 9812
Satellite: ISS
Catalog Number: 25544
Epoch time: 12116
53895470 = yrday
fracday
Element set: 912
Inclination: 51
6433 deg
RA of node: 25
7477 deg
Eccentricity:
0008232
Arg of perigee: 317
9099 deg
Mean anomaly: 42
1423 deg
Mean motion: 15
58597793 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 981
Checksum: 328
Coasting Arc #14 (Orbit 980)
---------------------------------------
Vector Time (GMT): 2012/116/12:23:02
249
Vector Time (MET): N/A
Weight (LBS) : 924784
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2488050
73 A = 6772507
18 meter
Y = -4766630
09 meter E =
0004241
Z = -4120238
04 I = 51
79136
XDOT = 6652
375665 Wp = 352
82492
YDOT = -171
764360 meter/sec RA = 25
33776 deg
ZDOT = -3813
867192 TA = 237
89633
MA = 237
93750
Ha = 214
176 n
mi
Hp = 212
734
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8162896
10 X = -2414548
93
Y = -15638550
16 feet Y = -4794041
98 meter
Z = -13517841
34 Z = -4132146
58
XDOT = 21825
379477 XDOT = 6672
329098
YDOT = -563
531366 feet/sec YDOT = -97
261757 meter/sec
ZDOT = -12512
687639 ZDOT = -3781
501356
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16106959
84 X = -4909401
36
Y = -7102820
29 feet Y = -2164939
62 meter
Z = -13566316
64 Z = -4135013
31
XDOT = 16177
256373 XDOT = 4930
827743
YDOT = -13011
588291 feet/sec YDOT = -3965
932111 meter/sec
ZDOT = -12379
666850 ZDOT = -3773
322456
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 12116
53897094
00016717 00000-0 10270-3 0 9137
2 25544 51
6442 25
7479 0007876 282
4490 77
5783 15
57418124 9818
Satellite: ISS
Catalog Number: 25544
Epoch time: 12116
53897094 = yrday
fracday
Element set: 913
Inclination: 51
6442 deg
RA of node: 25
7479 deg
Eccentricity:
0007876
Arg of perigee: 282
4490 deg
Mean anomaly: 77
5783 deg
Mean motion: 15
57418124 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 981
Checksum: 339
Coasting Arc #15 (Orbit 996)
---------------------------------------
Vector Time (GMT): 2012/117/12:23:02
249
Vector Time (MET): N/A
Weight (LBS) : 924784
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -464740
71 A = 6767952
25 meter
Y = 4245332
56 meter E =
0004756
Z = 5254402
49 I = 51
74804
XDOT = -7361
301180 Wp = 274
52453
YDOT = -1948
702866 meter/sec RA = 20
31971 deg
ZDOT = 924
462866 TA = 166
65383
MA = 166
64125
Ha = 214
399 n
mi
Hp = 212
639
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1524739
86 X = -537703
30
Y = 13928256
43 feet Y = 4239727
49 meter
Z = 17238853
31 Z = 5251967
63
XDOT = -24151
250589 XDOT = -7343
454154
YDOT = -6393
382105 feet/sec YDOT = -2030
921716 meter/sec
ZDOT = 3033
014653 ZDOT = 888
744942
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7677555
88 X = 2340119
03
Y = 11736075
43 feet Y = 3577155
79 meter
Z = 17228432
65 Z = 5251226
27
XDOT = -21793
442345 XDOT = -6642
641227
YDOT = 10024
916550 feet/sec YDOT = 3055
594564 meter/sec
ZDOT = 2886
426139 ZDOT = 879
782687
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 12117
56562859
00016717 00000-0 10270-3 0 9140
2 25544 51
6439 20
6041 0007932 285
7089 74
3190 15
57449515 9978
Satellite: ISS
Catalog Number: 25544
Epoch time: 12117
56562859 = yrday
fracday
Element set: 914
Inclination: 51
6439 deg
RA of node: 20
6041 deg
Eccentricity:
0007932
Arg of perigee: 285
7089 deg
Mean anomaly: 74
3190 deg
Mean motion: 15
57449515 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 997
Checksum: 332
Coasting Arc #16 (Orbit 1011)
---------------------------------------
Vector Time (GMT): 2012/118/12:23:02
249
Vector Time (MET): N/A
Weight (LBS) : 924784
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3438587
19 A = 6769339
01 meter
Y = -3101967
95 meter E =
0004279
Z = -4941283
63 I = 51
72408
XDOT = 6414
007392 Wp = 100
00908
YDOT = 3571
559310 meter/sec RA = 15
29182 deg
ZDOT = 2222
246297 TA = 191
64317
MA = 191
65307
Ha = 214
662 n
mi
Hp = 212
544
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11281454
03 X = 3497022
28
Y = -10177060
19 feet Y = -3063188
74 meter
Z = -16211560
47 Z = -4924437
11
XDOT = 21043
331340 XDOT = 6362
797533
YDOT = 11717
714272 feet/sec YDOT = 3642
998346 meter/sec
ZDOT = 7290
834308 ZDOT = 2253
281152
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1950668
98 X = 594563
91
Y = -15142268
79 feet Y = -4615363
53 meter
Z = -16142027
09 Z = -4920089
86
XDOT = 22444
249102 XDOT = 6841
007126
YDOT = -5013
266079 feet/sec YDOT = -1528
043501 meter/sec
ZDOT = 7418
017081 ZDOT = 2261
011606
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 12118
52810459
00016717 00000-0 10270-3 0 9150
2 25544 51
6442 15
7818 0008011 289
7248 70
3042 15
57465915 10122
Satellite: ISS
Catalog Number: 25544
Epoch time: 12118
52810459 = yrday
fracday
Element set: 915
Inclination: 51
6442 deg
RA of node: 15
7818 deg
Eccentricity:
0008011
Arg of perigee: 289
7248 deg
Mean anomaly: 70
3042 deg
Mean motion: 15
57465915 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1012
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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