[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
April 6th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15876 77 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 131 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 135 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 673)
---------------------------------------
Vector Time (GMT): 2012/096/20:03:41
679
Vector Time (MET): N/A
Weight (LBS) : 925359
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3264163
92 A = 6765961
24 meter
Y = 2623348
09 meter E =
0008713
Z = -5321040
92 I = 51
90969
XDOT = -4459
116305 Wp = 118
77159
YDOT = 6231
019580 meter/sec RA = 123
63723 deg
ZDOT = 332
883697 TA = 154
41136
MA = 154
36821
Ha = 214
046 n
mi
Hp = 211
307
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10709199
22 X = 3260435
14
Y = 8606785
08 feet Y = 2659828
47 meter
Z = -17457483
33 Z = -5305193
02
XDOT = -14629
646670 XDOT = -4530
078500
YDOT = 20442
977626 feet/sec YDOT = 6180
758254 meter/sec
ZDOT = 1092
138115 ZDOT = 311
048194
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1477456
13 X = -450328
63
Y = -13742045
97 feet Y = -4188575
61 meter
Z = -17392547
76 Z = -5301248
56
XDOT = 23827
411640 XDOT = 7262
595068
YDOT = -3845
315985 feet/sec YDOT = -1172
052312 meter/sec
ZDOT = 1002
039647 ZDOT = 305
421684
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 12096
85142454
00016717 00000-0 10270-3 0 9008
2 25544 51
6417 124
5142 0008022 243
8475 116
1855 15
58059209 6748
Satellite: ISS
Catalog Number: 25544
Epoch time: 12096
85142454 = yrday
fracday
Element set: 900
Inclination: 51
6417 deg
RA of node: 124
5142 deg
Eccentricity:
0008022
Arg of perigee: 243
8475 deg
Mean anomaly: 116
1855 deg
Mean motion: 15
58059209 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 674
Checksum: 300
Coasting Arc #2 (Orbit 689)
---------------------------------------
Vector Time (GMT): 2012/097/20:03:41
679
Vector Time (MET): N/A
Weight (LBS) : 925359
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1068311
74 A = 6769900
29 meter
Y = -5101565
90 meter E =
0001865
Z = 4318608
72 I = 51
93868
XDOT = 5412
435117 Wp = 90
29179
YDOT = -4131
411026 meter/sec RA = 118
62135 deg
ZDOT = -3540
228410 TA = 35
58059
MA = 35
56815
Ha = 213
781 n
mi
Hp = 211
346
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3504959
77 X = -1032164
69
Y = -16737420
93 feet Y = -5113309
84 meter
Z = 14168663
78 Z = 4313507
20
XDOT = 17757
333060 XDOT = 5475
428977
YDOT = -13554
498116 feet/sec YDOT = -4070
533996 meter/sec
ZDOT = -11614
922605 ZDOT = -3513
781247
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9136210
24 X = -2784716
88
Y = 14475483
12 feet Y = 4412127
26 meter
Z = 14148041
79 Z = 4312323
14
XDOT = -21167
368099 XDOT = -6451
813797
YDOT = -2109
875295 feet/sec YDOT = -643
089990 meter/sec
ZDOT = -11506
001623 ZDOT = -3507
029295
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 12097
87765420
00016717 00000-0 10270-3 0 9016
2 25544 51
6411 119
3678 0007995 248
1208 111
9097 15
58093183 6906
Satellite: ISS
Catalog Number: 25544
Epoch time: 12097
87765420 = yrday
fracday
Element set: 901
Inclination: 51
6411 deg
RA of node: 119
3678 deg
Eccentricity:
0007995
Arg of perigee: 248
1208 deg
Mean anomaly: 111
9097 deg
Mean motion: 15
58093183 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 690
Checksum: 326
Coasting Arc #3 (Orbit 704)
---------------------------------------
Vector Time (GMT): 2012/098/20:03:41
679
Vector Time (MET): N/A
Weight (LBS) : 925359
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1146453
52 A = 6776096
97 meter
Y = 6389942
60 meter E =
0004281
Z = -1932593
25 I = 51
97412
XDOT = -5150
367463 Wp = 311
22383
YDOT = 781
265173 meter/sec RA = 113
63334 deg
ZDOT = 5633
163690 TA = 27
54088
MA = 27
51820
Ha = 213
474 n
mi
Hp = 211
501
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3761330
45 X = -1208433
70
Y = 20964378
62 feet Y = 6376775
54 meter
Z = -6340529
03 Z = -1938313
83
XDOT = -16897
531046 XDOT = -5186
086002
YDOT = 2563
205947 feet/sec YDOT = 723
471326 meter/sec
ZDOT = 18481
508170 ZDOT = 5608
056227
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17105032
53 X = 5213613
92
Y = -12679373
59 feet Y = -3864673
07 meter
Z = -6364466
48 Z = -1939889
38
XDOT = 13199
020579 XDOT = 4023
061473
YDOT = 8572
260447 feet/sec YDOT = 2612
824984 meter/sec
ZDOT = 18378
304788 ZDOT = 5601
707299
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 12098
83972103
00016717 00000-0 10270-3 0 9022
2 25544 51
6417 114
5418 0008043 251
6023 108
4258 15
58136779 7056
Satellite: ISS
Catalog Number: 25544
Epoch time: 12098
83972103 = yrday
fracday
Element set: 902
Inclination: 51
6417 deg
RA of node: 114
5418 deg
Eccentricity:
0008043
Arg of perigee: 251
6023 deg
Mean anomaly: 108
4258 deg
Mean motion: 15
58136779 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 705
Checksum: 302
Coasting Arc #4 (Orbit 720)
---------------------------------------
Vector Time (GMT): 2012/099/20:03:41
679
Vector Time (MET): N/A
Weight (LBS) : 925359
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2927631
89 A = 6777245
11 meter
Y = -6007015
85 meter E =
0009858
Z = -1088700
91 I = 51
98928
XDOT = 3882
933416 Wp = 191
45039
YDOT = 2965
499314 meter/sec RA = 108
66751 deg
ZDOT = -5921
086785 TA =
32566
MA =
32502
Ha = 213
412 n
mi
Hp = 211
675
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9605091
52 X = 2999874
71
Y = -19708057
24 feet Y = -5973873
38 meter
Z = -3571853
39 Z = -1074302
61
XDOT = 12739
282862 XDOT = 3878
247750
YDOT = 9729
328458 feet/sec YDOT = 3008
894172 meter/sec
ZDOT = -19426
137745 ZDOT = -5902
234921
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20397694
46 X = -6217217
27
Y = 8063587
42 feet Y = 2457781
44 meter
Z = -3512272
55 Z = -1070540
67
XDOT = -2347
567267 XDOT = -715
538503
YDOT = -14365
865394 feet/sec YDOT = -4378
715772 meter/sec
ZDOT = -19348
892277 ZDOT = -5897
542366
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 12099
86590179
00016717 00000-0 10270-3 0 9036
2 25544 51
6419 109
3949 0008146 254
7491 105
2764 15
58126599 7210
Satellite: ISS
Catalog Number: 25544
Epoch time: 12099
86590179 = yrday
fracday
Element set: 903
Inclination: 51
6419 deg
RA of node: 109
3949 deg
Eccentricity:
0008146
Arg of perigee: 254
7491 deg
Mean anomaly: 105
2764 deg
Mean motion: 15
58126599 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 721
Checksum: 340
Coasting Arc #5 (Orbit 736)
---------------------------------------
Vector Time (GMT): 2012/100/20:03:41
679
Vector Time (MET): N/A
Weight (LBS) : 925359
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3994831
29 A = 6771607
80 meter
Y = 3964811
57 meter E =
0004573
Z = 3764216
39 I = 51
97995
XDOT = -1970
005431 Wp = 125
38497
YDOT = -6055
173691 meter/sec RA = 103
68932 deg
ZDOT = 4280
931516 TA = 279
49882
MA = 279
55050
Ha = 212
822 n
mi
Hp = 211
687
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13106401
85 X = -4057155
64
Y = 13007911
98 feet Y = 3919790
52 meter
Z = 12349791
32 Z = 3744657
96
XDOT = -6463
272410 XDOT = -1922
944886
YDOT = -19866
055416 feet/sec YDOT = -6076
940265 meter/sec
ZDOT = 14045
050907 ZDOT = 4271
475676
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18490345
87 X = 5635857
42
Y = -1037421
68 feet Y = -316206
13 meter
Z = 12269138
31 Z = 3739633
36
XDOT = -8304
365583 XDOT = -2531
170630
YDOT = 17881
841999 feet/sec YDOT = 5450
385441 meter/sec
ZDOT = 14006
639364 ZDOT = 4269
223678
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 12100
89205628
00016717 00000-0 10270-3 0 9045
2 25544 51
6422 104
2472 0007976 260
1211 99
9043 15
58184204 7373
Satellite: ISS
Catalog Number: 25544
Epoch time: 12100
89205628 = yrday
fracday
Element set: 904
Inclination: 51
6422 deg
RA of node: 104
2472 deg
Eccentricity:
0007976
Arg of perigee: 260
1211 deg
Mean anomaly: 99
9043 deg
Mean motion: 15
58184204 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 737
Checksum: 292
Coasting Arc #6 (Orbit 751)
---------------------------------------
Vector Time (GMT): 2012/101/20:03:41
679
Vector Time (MET): N/A
Weight (LBS) : 925359
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4245030
31 A = 6765850
21 meter
Y = -751866
99 meter E =
0006048
Z = -5219817
18 I = 51
96768
XDOT = -178
389111 Wp = 76
10111
YDOT = 7568
702051 meter/sec RA = 98
68125 deg
ZDOT = -1235
056933 TA = 182
10269
MA = 182
10523
Ha = 212
686 n
mi
Hp = 211
957
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13927264
79 X = 4278479
22
Y = -2466755
23 feet Y = -704209
49 meter
Z = -17125384
46 Z = -5199113
60
XDOT = -585
266111 XDOT = -257
010937
YDOT = 24831
699641 feet/sec YDOT = 7566
267578 meter/sec
ZDOT = -4052
024058 ZDOT = -1236
114616
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12281420
28 X = -3743376
90
Y = -7220035
16 feet Y = -2200666
72 meter
Z = -17040251
96 Z = -5193868
80
XDOT = 16002
450567 XDOT = 4877
546933
YDOT = -17643
842464 feet/sec YDOT = -5377
843183 meter/sec
ZDOT = -4056
938066 ZDOT = -1236
554723
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 12101
85405127
00016717 00000-0 10270-3 0 9059
2 25544 51
6422 99
4216 0008107 263
9633 96
0598 15
58260842 7523
Satellite: ISS
Catalog Number: 25544
Epoch time: 12101
85405127 = yrday
fracday
Element set: 905
Inclination: 51
6422 deg
RA of node: 99
4216 deg
Eccentricity:
0008107
Arg of perigee: 263
9633 deg
Mean anomaly: 96
0598 deg
Mean motion: 15
58260842 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 752
Checksum: 306
Coasting Arc #7 (Orbit 767)
---------------------------------------
Vector Time (GMT): 2012/102/20:03:41
679
Vector Time (MET): N/A
Weight (LBS) : 925359
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3709166
61 A = 6766811
08 meter
Y = -2737172
89 meter E =
0004148
Z = 4957180
20 I = 51
97554
XDOT = 2192
797036 Wp = 318
34900
YDOT = -7006
923359 meter/sec RA = 93
66120 deg
ZDOT = -2226
269511 TA = 153
27630
MA = 153
25492
Ha = 211
967 n
mi
Hp = 211
421
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12169181
79 X = -3702364
25
Y = -8980226
01 feet Y = -2778612
99 meter
Z = 16263714
58 Z = 4939177
74
XDOT = 7194
215997 XDOT = 2281
801647
YDOT = -22988
593698 feet/sec YDOT = -6981
904522 meter/sec
ZDOT = -7304
033829 ZDOT = -2215
400694
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3770098
85 X = 1149126
13
Y = 14728000
05 feet Y = 4489094
42 meter
Z = 16189942
11 Z = 4934694
36
XDOT = -19120
427885 XDOT = -5827
906419
YDOT = 12880
925128 feet/sec YDOT = 3926
105979 meter/sec
ZDOT = -7258
830119 ZDOT = -2212
491420
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 12102
88015447
00016717 00000-0 10270-3 0 9066
2 25544 51
6427 94
2745 0008207 267
7370 92
2845 15
58314327 7687
Satellite: ISS
Catalog Number: 25544
Epoch time: 12102
88015447 = yrday
fracday
Element set: 906
Inclination: 51
6427 deg
RA of node: 94
2745 deg
Eccentricity:
0008207
Arg of perigee: 267
7370 deg
Mean anomaly: 92
2845 deg
Mean motion: 15
58314327 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 768
Checksum: 317
Coasting Arc #8 (Orbit 782)
---------------------------------------
Vector Time (GMT): 2012/103/20:03:41
679
Vector Time (MET): N/A
Weight (LBS) : 925359
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2509015
32 A = 6773275
12 meter
Y = 5502061
76 meter E =
0004287
Z = -3045703
10 I = 51
99738
XDOT = -3775
316430 Wp = 292
51640
YDOT = 4471
698354 meter/sec RA = 88
66131 deg
ZDOT = 4964
112826 TA = 32
67343
MA = 32
64692
Ha = 211
880 n
mi
Hp = 211
527
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8231677
55 X = 2462099
01
Y = 18051383
72 feet Y = 5529856
73 meter
Z = -9992464
23 Z = -3033628
49
XDOT = -12386
208760 XDOT = -3849
153809
YDOT = 14670
926358 feet/sec YDOT = 4429
067690 meter/sec
ZDOT = 16286
459404 ZDOT = 4945
593070
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4731878
57 X = 1442276
59
Y = -19292564
32 feet Y = -5880373
61 meter
Z = -9943268
98 Z = -3030708
38
XDOT = 17494
514471 XDOT = 5332
328011
YDOT = -4070
367274 feet/sec YDOT = -1240
647945 meter/sec
ZDOT = 16209
996885 ZDOT = 4940
807051
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 12103
84210371
00016717 00000-0 10270-3 0 9077
2 25544 51
6420 89
4481 0008241 271
3408 88
6803 15
58313296 7838
Satellite: ISS
Catalog Number: 25544
Epoch time: 12103
84210371 = yrday
fracday
Element set: 907
Inclination: 51
6420 deg
RA of node: 89
4481 deg
Eccentricity:
0008241
Arg of perigee: 271
3408 deg
Mean anomaly: 88
6803 deg
Mean motion: 15
58313296 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 783
Checksum: 299
Coasting Arc #9 (Orbit 798)
---------------------------------------
Vector Time (GMT): 2012/104/20:03:41
679
Vector Time (MET): N/A
Weight (LBS) : 925359
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -823595
11 A = 6777145
89 meter
Y = -6720686
55 meter E =
0008003
Z = 102632
87 I = 52
00863
XDOT = 4678
684856 Wp = 174
18752
YDOT = -666
219701 meter/sec RA = 83
69178 deg
ZDOT = -6047
757306 TA = 4
71056
MA = 4
70303
Ha = 212
009 n
mi
Hp = 211
484
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2702083
70 X = -748880
39
Y = -22049496
55 feet Y = -6729478
74 meter
Z = 336722
02 Z = 98813
63
XDOT = 15350
015931 XDOT = 4715
165503
YDOT = -2185
760174 feet/sec YDOT = -613
696006 meter/sec
ZDOT = -19841
723444 ZDOT = -6024
939883
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11267100
14 X = -3434212
12
Y = 19145338
64 feet Y = 5835499
22 meter
Z = 321556
95 Z = 98010
56
XDOT = -12212
886186 XDOT = -3722
487710
YDOT = -6853
731060 feet/sec YDOT = -2089
017227 meter/sec
ZDOT = -19747
889962 ZDOT = -6019
156861
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
86815694
00016717 00000-0 10270-3 0 9080
2 25544 51
6419 84
3010 0008139 273
9068 86
1157 15
58327819 7992
Satellite: ISS
Catalog Number: 25544
Epoch time: 12104
86815694 = yrday
fracday
Element set: 908
Inclination: 51
6419 deg
RA of node: 84
3010 deg
Eccentricity:
0008139
Arg of perigee: 273
9068 deg
Mean anomaly: 86
1157 deg
Mean motion: 15
58327819 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 799
Checksum: 336
Coasting Arc #10 (Orbit 814)
---------------------------------------
Vector Time (GMT): 2012/105/20:03:41
679
Vector Time (MET): N/A
Weight (LBS) : 925359
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1097119
88 A = 6773395
31 meter
Y = 6025314
91 meter E =
0005934
Z = 2884634
99 I = 51
99157
XDOT = -4710
334375 Wp = 56
88803
YDOT = -3294
781038 meter/sec RA = 78
72094 deg
ZDOT = 5086
149418 TA = 335
85015
MA = 335
87796
Ha = 212
597 n
mi
Hp = 211
605
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3599474
68 X = -1178427
51
Y = 19768093
53 feet Y = 6012591
78 meter
Z = 9464025
56 Z = 2879107
42
XDOT = -15453
852936 XDOT = -4697
848690
YDOT = -10809
649074 feet/sec YDOT = -3347
384816 meter/sec
ZDOT = 16686
841922 ZDOT = 5063
297393
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14694442
42 X = 4478866
05
Y = -13720267
57 feet Y = -4181937
55 meter
Z = 9440823
03 Z = 2877562
86
XDOT = 5079
587977 XDOT = 1548
258415
YDOT = 16867
797833 feet/sec YDOT = 5141
304780 meter/sec
ZDOT = 16593
180793 ZDOT = 5057
601506
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
89418074
00016717 00000-0 10270-3 0 9096
2 25544 51
6410 79
1516 0008292 278
4807 81
5408 15
58405578 8153
Satellite: ISS
Catalog Number: 25544
Epoch time: 12105
89418074 = yrday
fracday
Element set: 909
Inclination: 51
6410 deg
RA of node: 79
1516 deg
Eccentricity:
0008292
Arg of perigee: 278
4807 deg
Mean anomaly: 81
5408 deg
Mean motion: 15
58405578 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 815
Checksum: 323
Coasting Arc #11 (Orbit 829)
---------------------------------------
Vector Time (GMT): 2012/106/20:03:41
679
Vector Time (MET): N/A
Weight (LBS) : 925359
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2928697
17 A = 6766688
62 meter
Y = -3642250
03 meter E =
0006220
Z = -4898197
67 I = 51
96114
XDOT = 3767
107524 Wp = 33
26257
YDOT = 6242
075194 meter/sec RA = 73
72128 deg
ZDOT = -2385
502323 TA = 213
46171
MA = 213
50102
Ha = 212
729 n
mi
Hp = 211
517
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9608586
50 X = 2993002
20
Y = -11949639
21 feet Y = -3609140
33 meter
Z = -16070202
34 Z = -4883813
75
XDOT = 12359
276653 XDOT = 3708
615618
YDOT = 20479
249323 feet/sec YDOT = 6283
874103 meter/sec
ZDOT = -7826
451190 ZDOT = -2367
344420
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14841455
66 X = -4523675
68
Y = 4093427
38 feet Y = 1247676
67 meter
Z = -16010785
78 Z = -4880087
51
XDOT = 2089
078868 XDOT = 636
751239
YDOT = -22794
510190 feet/sec YDOT = -6947
766706 meter/sec
ZDOT = -7752
326310 ZDOT = -2362
909059
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
85605457
00016717 00000-0 10270-3 0 9108
2 25544 51
6397 74
3248 0008225 281
7682 78
2550 15
58436322 8309
Satellite: ISS
Catalog Number: 25544
Epoch time: 12106
85605457 = yrday
fracday
Element set: 910
Inclination: 51
6397 deg
RA of node: 74
3248 deg
Eccentricity:
0008225
Arg of perigee: 281
7682 deg
Mean anomaly: 78
2550 deg
Mean motion: 15
58436322 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 830
Checksum: 311
Coasting Arc #12 (Orbit 845)
---------------------------------------
Vector Time (GMT): 2012/107/20:03:41
679
Vector Time (MET): N/A
Weight (LBS) : 925359
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4282834
41 A = 6765193
69 meter
Y = 292758
71 meter E =
0006333
Z = 5233441
10 I = 51
94728
XDOT = -1902
960685 Wp = 312
41880
YDOT = -7343
535399 meter/sec RA = 68
69770 deg
ZDOT = -1143
223388 TA = 148
50871
MA = 148
47078
Ha = 212
838 n
mi
Hp = 211
189
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14051293
98 X = -4311212
72
Y = 960494
45 feet Y = 244707
16 meter
Z = 17170082
35 Z = 5212566
28
XDOT = -6243
309334 XDOT = -1815
148815
YDOT = -24092
963907 feet/sec YDOT = -7364
324593 meter/sec
ZDOT = -3750
732900 ZDOT = -1152
254014
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12208976
16 X = 3721295
93
Y = 7227869
89 feet Y = 2203054
74 meter
Z = 17084259
95 Z = 5207282
43
XDOT = -7997
894949 XDOT = -2437
758380
YDOT = 22487
039684 feet/sec YDOT = 6854
049696 meter/sec
ZDOT = -3787
244201 ZDOT = -1154
352032
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
88202650
00016717 00000-0 10270-3 0 9111
2 25544 51
6402 69
1761 0008203 284
9695 75
0552 15
58465989 8468
Satellite: ISS
Catalog Number: 25544
Epoch time: 12107
88202650 = yrday
fracday
Element set: 911
Inclination: 51
6402 deg
RA of node: 69
1761 deg
Eccentricity:
0008203
Arg of perigee: 284
9695 deg
Mean anomaly: 75
0552 deg
Mean motion: 15
58465989 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 846
Checksum: 323
Coasting Arc #13 (Orbit 860)
---------------------------------------
Vector Time (GMT): 2012/108/20:03:41
679
Vector Time (MET): N/A
Weight (LBS) : 925359
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4764461
89 A = 6770655
39 meter
Y = 3000278
47 meter E =
0002438
Z = -3757418
30 I = 51
95305
XDOT = -608
893584 Wp = 302
63469
YDOT = 6336
541507 meter/sec RA = 63
68377 deg
ZDOT = 4286
876547 TA = 12
54636
MA = 12
54029
Ha = 213
017 n
mi
Hp = 210
981
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15631436
64 X = 4748810
87
Y = 9843433
29 feet Y = 3053469
80 meter
Z = -12327487
86 Z = -3734310
88
XDOT = -1997
682362 XDOT = -700
529636
YDOT = 20789
178174 feet/sec YDOT = 6329
220479 meter/sec
ZDOT = 14064
555600 ZDOT = 4283
695433
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7656827
32 X = -2333800
97
Y = -16879998
42 feet Y = -5145023
52 meter
Z = -12232767
32 Z = -3728547
48
XDOT = 11988
381041 XDOT = 3654
058541
YDOT = -15622
309781 feet/sec YDOT = -4761
680021 meter/sec
ZDOT = 14050
949534 ZDOT = 4282
729418
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
84384937
00016717 00000-0 10270-3 0 9128
2 25544 51
6392 64
3477 0008155 288
0986 71
9280 15
58522659 8619
Satellite: ISS
Catalog Number: 25544
Epoch time: 12108
84384937 = yrday
fracday
Element set: 912
Inclination: 51
6392 deg
RA of node: 64
3477 deg
Eccentricity:
0008155
Arg of perigee: 288
0986 deg
Mean anomaly: 71
9280 deg
Mean motion: 15
58522659 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 861
Checksum: 341
Coasting Arc #14 (Orbit 876)
---------------------------------------
Vector Time (GMT): 2012/109/20:03:41
679
Vector Time (MET): N/A
Weight (LBS) : 925359
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4100519
00 A = 6775971
79 meter
Y = -5304594
26 meter E =
0005671
Z = 956292
45 I = 51
95791
XDOT = 3259
350502 Wp = 142
49373
YDOT = -3593
842475 meter/sec RA = 58
70329 deg
ZDOT = -5945
244257 TA = 27
17788
MA = 27
14821
Ha = 213
035 n
mi
Hp = 210
614
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13453146
33 X = -4045542
69
Y = -17403524
47 feet Y = -5350141
33 meter
Z = 3137442
41 Z = 936506
06
XDOT = 10693
407159 XDOT = 3328
176290
YDOT = -11790
821767 feet/sec YDOT = -3557
010047 meter/sec
ZDOT = -19505
394543 ZDOT = -5929
242853
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1995818
94 X = 608325
61
Y = 21917741
81 feet Y = 6680527
70 meter
Z = 3056575
77 Z = 931644
29
XDOT = -13859
068223 XDOT = -4224
243994
YDOT = 3979
551688 feet/sec YDOT = 1212
967354 meter/sec
ZDOT = -19439
323021 ZDOT = -5925
105657
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
86976563
00016717 00000-0 10270-3 0 9134
2 25544 51
6399 59
1994 0008302 293
0899 66
9380 15
58606597 8771
Satellite: ISS
Catalog Number: 25544
Epoch time: 12109
86976563 = yrday
fracday
Element set: 913
Inclination: 51
6399 deg
RA of node: 59
1994 deg
Eccentricity:
0008302
Arg of perigee: 293
0899 deg
Mean anomaly: 66
9380 deg
Mean motion: 15
58606597 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 877
Checksum: 369
Coasting Arc #15 (Orbit 892)
---------------------------------------
Vector Time (GMT): 2012/110/20:03:41
679
Vector Time (MET): N/A
Weight (LBS) : 925359
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2268874
14 A = 6774272
27 meter
Y = 5988911
68 meter E =
0009787
Z = 2188166
24 I = 51
93485
XDOT = -5345
914313 Wp = 36
19879
YDOT = 9
864612 meter/sec RA = 53
73131 deg
ZDOT = 5511
284355 TA = 348
04783
MA = 348
07104
Ha = 213
076 n
mi
Hp = 210
425
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7443812
78 X = 2191106
52
Y = 19648660
36 feet Y = 6013848
96 meter
Z = 7179023
10 Z = 2198999
17
XDOT = -17539
088955 XDOT = -5372
400247
YDOT = 32
364213 feet/sec YDOT = -50
064423 meter/sec
ZDOT = 18081
641585 ZDOT = 5485
249451
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3976841
18 X = 1212141
19
Y = -20616286
60 feet Y = -6283844
16 meter
Z = 7223021
28 Z = 2201576
89
XDOT = 13553
278543 XDOT = 4131
039300
YDOT = 8917
402510 feet/sec YDOT = 2718
024285 meter/sec
ZDOT = 17974
643294 ZDOT = 5478
671276
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
89565602
00016717 00000-0 10270-3 0 9148
2 25544 51
6391 54
0492 0008085 294
8354 65
1960 15
58608570 8939
Satellite: ISS
Catalog Number: 25544
Epoch time: 12110
89565602 = yrday
fracday
Element set: 914
Inclination: 51
6391 deg
RA of node: 54
0492 deg
Eccentricity:
0008085
Arg of perigee: 294
8354 deg
Mean anomaly: 65
1960 deg
Mean motion: 15
58608570 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 893
Checksum: 321
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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